{"id":578,"date":"2018-05-19T21:02:57","date_gmt":"2018-05-19T21:02:57","guid":{"rendered":"http:\/\/www.uprm.edu\/hpcvl\/?page_id=14"},"modified":"2024-04-26T18:57:41","modified_gmt":"2024-04-26T18:57:41","slug":"research","status":"publish","type":"page","link":"https:\/\/ceid.utsa.edu\/garaya\/research\/","title":{"rendered":"Research"},"content":{"rendered":"[et_pb_section fb_built=&#8221;1&#8243; admin_label=&#8221;Section&#8221; _builder_version=&#8221;3.22&#8243;][et_pb_row admin_label=&#8221;Row&#8221; _builder_version=&#8221;3.25&#8243; background_size=&#8221;initial&#8221; background_position=&#8221;top_left&#8221; background_repeat=&#8221;repeat&#8221;][et_pb_column type=&#8221;4_4&#8243; _builder_version=&#8221;3.25&#8243; custom_padding=&#8221;|||&#8221; custom_padding__hover=&#8221;|||&#8221;][et_pb_text admin_label=&#8221;Text&#8221; _builder_version=&#8221;4.9.7&#8243; header_text_color=&#8221;#000000&#8243; background_size=&#8221;initial&#8221; background_position=&#8221;top_left&#8221; background_repeat=&#8221;repeat&#8221; text_orientation=&#8221;center&#8221; module_alignment=&#8221;center&#8221; use_border_color=&#8221;off&#8221; border_color=&#8221;#ffffff&#8221; border_style=&#8221;solid&#8221;]\n<h1 style=\"text-align: center\">Flow Animation and Research Projects<\/h1>\n<p>Scientific visualization of high spatial\/temporal resolution numerical simulations (i.e. DNS or LES) is carried out. In addition, mixed reality (MR) has been implemented by the development of a Virtual Wind Tunnel (VWT) and making use of Virtual and Augmented Reality (VR\/AR) of static and dynamic frames. In addition, readers can access to important information regarding our current\/past research projects. Enjoy!<\/p>\n[\/et_pb_text][\/et_pb_column][\/et_pb_row][et_pb_row admin_label=&#8221;Row&#8221; _builder_version=&#8221;3.25&#8243; background_size=&#8221;initial&#8221; background_position=&#8221;top_left&#8221; background_repeat=&#8221;repeat&#8221;][et_pb_column type=&#8221;4_4&#8243; _builder_version=&#8221;3.25&#8243; custom_padding=&#8221;|||&#8221; custom_padding__hover=&#8221;|||&#8221;][et_pb_video_slider controls_color=&#8221;light&#8221; disabled_on=&#8221;off|off|off&#8221; admin_label=&#8221;Video Slider&#8221; _builder_version=&#8221;4.9.7&#8243; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;][et_pb_video_slider_item admin_title=&#8221;\tDNS of supersonic turbulent boundary layers subject to strong concave\/convex curvatures&#8221; src=&#8221;https:\/\/youtu.be\/LFQ4g1DWvm8?si=6kNTker1PArEJxSe&#8221; image_src=&#8221;\/\/i.ytimg.com\/vi\/ZGXU56ZvPwQ\/hqdefault.jpg&#8221; _builder_version=&#8221;4.9.7&#8243; hover_enabled=&#8221;0&#8243; show_image_overlay=&#8221;off&#8221; sticky_enabled=&#8221;0&#8243;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;APS-GFM-2022 V0026&#8243; src=&#8221;https:\/\/youtu.be\/My9WH9RiyxU&#8221; _builder_version=&#8221;4.9.7&#8243; _module_preset=&#8221;default&#8221; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;APS-GFM-2022 V0026&#8243; src=&#8221;https:\/\/www.youtube.com\/watch?v=9FaqTyt5vGY&#8221; _builder_version=&#8221;4.9.7&#8243; _module_preset=&#8221;default&#8221; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;APS-GFM-2021 V0027&#8243; src=&#8221;https:\/\/www.youtube.com\/watch?v=Au6Sa-E0R3Q&#8221; _builder_version=&#8221;4.9.7&#8243; _module_preset=&#8221;default&#8221; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;APS-GFM-2022 V0025&#8243; src=&#8221;https:\/\/youtu.be\/-MLsfKImNy4&#8243; _builder_version=&#8221;4.9.7&#8243; _module_preset=&#8221;default&#8221; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;APS-GFM Video45 2020&#8243; src=&#8221;https:\/\/youtu.be\/jQB_YxK5_q4&#8243; image_src=&#8221;\/\/i.ytimg.com\/vi\/Q_PsKz8Q4U0\/hqdefault.jpg&#8221; _builder_version=&#8221;4.9.7&#8243; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;APS-GFM-2021 V0028&#8243; src=&#8221;https:\/\/www.youtube.com\/watch?v=E1IM5gJDAsg&amp;t=2s&#8221; _builder_version=&#8221;4.9.7&#8243; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;APS-GFM Video40 2020&#8243; src=&#8221;https:\/\/www.youtube.com\/watch?v=Q_PsKz8Q4U0&#8243; image_src=&#8221;\/\/i.ytimg.com\/vi\/Q_PsKz8Q4U0\/hqdefault.jpg&#8221; _builder_version=&#8221;4.9.7&#8243; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;VR Jean&#8221; src=&#8221;https:\/\/youtu.be\/M6MGwgdvVkY&#8221; _builder_version=&#8221;3.0.47&#8243; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;VWT&#8221; src=&#8221;https:\/\/www.youtube.com\/watch?v=-O2HP9mgH0k&#8221; image_src=&#8221;https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2020\/08\/first_slide.png&#8221; _builder_version=&#8221;3.0.47&#8243; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;Supersonic Concave Convex&#8221; src=&#8221;https:\/\/fluid.colorado.edu\/~kjansen\/Weblink\/QandT240MB.mov&#8221; image_src=&#8221;https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2019\/10\/Video_KJ_M2_5_V2.png&#8221; _builder_version=&#8221;3.0.47&#8243; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;Supersonic Concave Convex (CL)&#8221; src=&#8221;https:\/\/www.youtube.com\/watch?v=U2DyCZ4TVrg&#8221; image_src=&#8221;\/\/i.ytimg.com\/vi\/U2DyCZ4TVrg\/hqdefault.jpg&#8221; _builder_version=&#8221;4.9.7&#8243; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;GFM 2019&#8243; src=&#8221;https:\/\/youtu.be\/uzUarMZSpWM&#8221; _builder_version=&#8221;3.0.47&#8243; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;Crossfow jet VR=1&#8243; src=&#8221;https:\/\/youtu.be\/CaYTJzENpuA&#8221; image_src=&#8221;https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2019\/12\/movieVR1_HR_image.png&#8221; _builder_version=&#8221;3.0.47&#8243; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;APS-GFM Video 21 2018&#8243; src=&#8221;https:\/\/youtu.be\/bwyfJMwFiL0&#8243; _builder_version=&#8221;4.9.7&#8243; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][et_pb_video_slider_item admin_title=&#8221;Quasi-laminarization (Jean Santiago)&#8221; src=&#8221;https:\/\/youtu.be\/LaUYJ6NBKwE&#8221; _builder_version=&#8221;4.9.7&#8243; show_image_overlay=&#8221;off&#8221;] [\/et_pb_video_slider_item][\/et_pb_video_slider][\/et_pb_column][\/et_pb_row][et_pb_row admin_label=&#8221;Row&#8221; _builder_version=&#8221;3.25&#8243; background_size=&#8221;initial&#8221; background_position=&#8221;top_left&#8221; background_repeat=&#8221;repeat&#8221;][et_pb_column type=&#8221;4_4&#8243; _builder_version=&#8221;3.25&#8243; custom_padding=&#8221;|||&#8221; custom_padding__hover=&#8221;|||&#8221;][et_pb_accordion admin_label=&#8221;Accordion&#8221; _builder_version=&#8221;4.9.7&#8243; hover_enabled=&#8221;0&#8243; use_border_color=&#8221;off&#8221; border_color=&#8221;#ffffff&#8221; border_style=&#8221;solid&#8221; sticky_enabled=&#8221;0&#8243;][et_pb_accordion_item title=&#8221;Coherent structure assessment in high-speed crossflow jets (Award #FA9550-23-1-0241)&#8221; open=&#8221;on&#8221; _builder_version=&#8221;4.9.7&#8243;]\n<p style=\"text-align: center\">Guillermo Araya<sup>1<\/sup>and Kenneth Jansen<sup>2<\/sup><\/p>\n<p style=\"text-align: center\"><sup>1<\/sup>Department of Mechanical Engineering, University of Puerto Rico at Mayagez (UPRM), PR 00681<\/p>\n<p style=\"text-align: center\"><sup>2<\/sup>Department of Aerospace Engineering Sciences, University of Colorado at Boulder (UCB), CO 80309<\/p>\n<h2><strong>Introduction<\/strong><\/h2>\n<p><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">Compressible jets transversely issuing into a spatially-developing turbulent boundary layer (SDTBL) are one of the most challenging types of\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">three-dimensional flows due to their thermal-fluid complexity and technological applications; for instance, film cooling of turbine blades, fuel\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">or dilution air injection in gas turbine engines, thrust vector control, just to name a few. The ability to control a flow field in such a way to\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">enhance thermal efficiency is of crucial relevance in aerospace and other engineering applications. We seek to perform Direct Numerical\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">Simulation (DNS) with high spatial and temporal resolution of high-speed jets in crossflow at high Reynolds numbers. The analysis will be\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">done by prescribing accurate turbulent flow information (instantaneous velocity, temperature and pressure) at the inlet of the computational\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">domain for simulations of SDTBL based on the Dynamic-Multiscale Approach (DMA) by Araya et al. [1], and more recently extended to\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">supersonic\/hypersonic flow [2, 3, 4, 5]. Extensive DNS cases are planned (sonic jets interacting with supersonic crossflow and supersonic\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">jets issuing into subsonic or hypersonic crossflow at different flow conditions) by reproducing wind tunnel studies as in [6] and [7] for\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">numerical validation. Furthermore, the extensive data supplied by DNS will allow us to elucidate the jet-SDTBL interaction on the complex\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">vortex system (or coherent structures) generated downstream and to gain a better knowledge on the different processes of the vorticity\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">transport (such as stretching, tilting and diffusion). Furthermore, the proposed flow solver (the PHASTA project, led by Dr. Jansen)\u00a0<\/span><span class=\"AdvancedProofingIssue SCXP10690726 BCX8\">is able to<\/span><span class=\"NormalTextRun SCXP10690726 BCX8\">\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">simulate complex geometries and has shown a great scalability for\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"SpellingError SCXP10690726 BCX8\">petascale<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">\u00a0computing on the Argonne Leadership Computing Facility\u2019s\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">Blue Gene\/Q Mira with up to 786,432 cores [8] and is being extended to\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"SpellingError SCXP10690726 BCX8\">exascale<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">\u00a0[9] under two Aurora Early Science Projects. The main\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">research objectives of the proposed body of work are three-fold. The first goal involves DNS of high-speed jets in crossflow at high Reynolds\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">numbers and computation\/validation of low\/high order statistics of flow parameters, intermittency, energy budget and power\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">spectra\/<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"SpellingError SCXP10690726 BCX8\">cospectra<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">\u00a0of the jet-SDTBL interaction. The second goal consists\u00a0<\/span><span class=\"ContextualSpellingAndGrammarError SCXP10690726 BCX8\">on<\/span><span class=\"NormalTextRun SCXP10690726 BCX8\">\u00a0a better and more objective understanding of the physics\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">behind\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"SpellingError SCXP10690726 BCX8\">Lagrangian<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">\u00a0coherent motions emanating from crossflow jets. The third goal consists of high-end visualization of the transport\u00a0<\/span><\/span><span class=\"TextRun SCXP10690726 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP10690726 BCX8\">phenomena via flow animation videos and Virtual\/Augmented Reality (VR\/AR).<\/span><\/span><span class=\"EOP SCXP10690726 BCX8\">\u200b<\/span><\/p>\n<p>&nbsp;<\/p>\n<h2><strong>Intellectual Merit <\/strong><\/h2>\n<p><span class=\"EOP SCXP10690726 BCX8\"><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">The high spatial\/temporal resolution and numerical accuracy of DNS, combined with the objective mathematical\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">framework of the\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"SpellingError SCXP79033270 BCX8\">Lagrangian<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">\u00a0Coherent Structure (LCS) approach, will shed important light on the physics behind the\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">complex set of flow structures in compressible crossflow jets, lambda\/bow\/barrel shock formation, Mach disk and jet\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">boundaries. Furthermore, DNS is a numerical technique that resolves all turbulence length\/time scales, and thus, it is\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">superior in terms of information provided by any other numerical technique. The prescribed friction Reynolds numbers\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">will be high enough to allow a noticeable separation of turbulent scales (i.e.,\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">\u03b4<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun Superscript SCXP79033270 BCX8\" data-fontsize=\"18\">+<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">\u00a0= \u03b4\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"SpellingError SCXP79033270 BCX8\">u<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"SpellingError Subscript SCXP79033270 BCX8\" data-fontsize=\"18\">\u03c4<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">\u00a0\/<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"SpellingError SCXP79033270 BCX8\">\u03bd<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"SpellingError Subscript SCXP79033270 BCX8\" data-fontsize=\"18\">w<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">&gt; 1,000) with the purpose of\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">\u201cpushing the envelope\u201d of DNS at higher Reynolds numbers in high-speed crossflow jets. In addition, DNS will supply\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">important insight in regions unreachable by experiments, such as the very near wall region where velocity\/thermal\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">gradients play a crucial role on the transport phenomena. To our knowledge, the proposed\u00a0<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"SpellingError SCXP79033270 BCX8\">petascale<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">\u00a0DNS study on high-<\/span><\/span><span class=\"TextRun SCXP79033270 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP79033270 BCX8\">speed crossflow jets and high Reynolds numbers will be carried out for the first time.<\/span><\/span>\u200b<\/span><\/p>\n<p><strong>\u00a0<\/strong><\/p>\n<h2><strong>Broader Impact<\/strong><\/h2>\n<p><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP264308028 BCX8\">The proposed study, based on DNS big data, will contribute to a better understanding of coherent structures and thermal\u00a0<\/span><\/span><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP264308028 BCX8\">transport in compressible crossflow jets. This would also lead to the improvement of flow control tools for mixing\u00a0<\/span><\/span><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP264308028 BCX8\">enhancement, drag reduction, heat transfer augmentation and noise reduction. Moreover, the data obtained from\u00a0<\/span><\/span><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP264308028 BCX8\">extensive DNS, will be shared with the entire fluid dynamics community. In addition, the project will have several\u00a0<\/span><\/span><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP264308028 BCX8\">educational\/outreach components including:\u00a0<\/span><\/span><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"SpellingError SCXP264308028 BCX8\">i<\/span><\/span><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP264308028 BCX8\">) recruitment of graduate students at UPRM and UCB as research\u00a0<\/span><\/span><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP264308028 BCX8\">assistants, where underrepresented minorities will be targeted during the hiring process, ii) provision of adequate\u00a0<\/span><\/span><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP264308028 BCX8\">coaching for advanced research in the field of thermal-fluid sciences with emphasis on modeling, data analysis, parallel\u00a0<\/span><\/span><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP264308028 BCX8\">computing and scientific visualization, iv) dissemination of outcomes in peer-reviewed articles and conferences, v)\u00a0<\/span><\/span><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP264308028 BCX8\">establishment of a fruitful research collaboration between UTSA and UCB, with periodic virtual meetings in order to\u00a0<\/span><\/span><span class=\"TextRun SCXP264308028 BCX8\" lang=\"EN-US\" xml:lang=\"EN-US\" data-usefontface=\"true\" data-contrast=\"none\"><span class=\"NormalTextRun SCXP264308028 BCX8\">leverage the skills of participants; and, at the same time, to promote diversity.<\/span><\/span><span class=\"EOP SCXP264308028 BCX8\">\u200b<\/span><\/p>\n<p><img fetchpriority=\"high\" fetchpriority=\"high\" decoding=\"async\" class=\"aligncenter wp-image-1136 size-large\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Picture1-1024x335.png\" alt=\"\" width=\"1024\" height=\"335\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Picture1-980x321.png 980w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Picture1-480x157.png 480w\" sizes=\"(min-width: 0px) and (max-width: 480px) 480px, (min-width: 481px) and (max-width: 980px) 980px, (min-width: 981px) 1024px, 100vw\" \/><\/p>\n<p style=\"text-align: center\">(*) The image shows iso-surfaces of vortex cores (Q-criterion) via DNS colored by the local Mach number in a subsonic crossflow (Mach 0.8) and a supersonic jet (Mach 3.73)<\/p>\n<p><img decoding=\"async\" class=\"aligncenter wp-image-1137 size-full\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145005.png\" alt=\"\" width=\"838\" height=\"469\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145005.png 838w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145005-480x269.png 480w\" sizes=\"(min-width: 0px) and (max-width: 480px) 480px, (min-width: 481px) 838px, 100vw\" \/><\/p>\n<p>&nbsp;<\/p>\n<p><img decoding=\"async\" class=\"aligncenter wp-image-1138 size-large\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145031-1024x574.png\" alt=\"\" width=\"1024\" height=\"574\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145031-980x549.png 980w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145031-480x269.png 480w\" sizes=\"(min-width: 0px) and (max-width: 480px) 480px, (min-width: 481px) and (max-width: 980px) 980px, (min-width: 981px) 1024px, 100vw\" \/><\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" class=\"aligncenter wp-image-1139 size-large\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145047-1024x574.png\" alt=\"\" width=\"1024\" height=\"574\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145047-980x549.png 980w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145047-480x269.png 480w\" sizes=\"auto, (min-width: 0px) and (max-width: 480px) 480px, (min-width: 481px) and (max-width: 980px) 980px, (min-width: 981px) 1024px, 100vw\" \/><\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" class=\"aligncenter wp-image-1140 size-large\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145112-1024x575.png\" alt=\"\" width=\"1024\" height=\"575\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145112-980x550.png 980w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145112-480x269.png 480w\" sizes=\"auto, (min-width: 0px) and (max-width: 480px) 480px, (min-width: 481px) and (max-width: 980px) 980px, (min-width: 981px) 1024px, 100vw\" \/><\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" class=\"aligncenter wp-image-1146 size-large\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145741-1024x576.png\" alt=\"\" width=\"1024\" height=\"576\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145741-980x551.png 980w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145741-480x270.png 480w\" sizes=\"auto, (min-width: 0px) and (max-width: 480px) 480px, (min-width: 481px) and (max-width: 980px) 980px, (min-width: 981px) 1024px, 100vw\" \/><\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" class=\"aligncenter wp-image-1145 size-large\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145635-1024x577.png\" alt=\"\" width=\"1024\" height=\"577\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145635-980x552.png 980w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2024\/01\/Screenshot-2024-01-10-145635-480x271.png 480w\" sizes=\"auto, (min-width: 0px) and (max-width: 480px) 480px, (min-width: 481px) and (max-width: 980px) 980px, (min-width: 981px) 1024px, 100vw\" \/><\/p>\n<p>&nbsp;<\/p>\n<p><strong>References<\/strong><\/p>\n[1] G. Araya, L. Castillo, C. Meneveau, and K. Jansen, \u201c A dynamic multi-scale approach for turbulent inflow boundary conditions in spatially evolving flows,\u201d Journal of Fluid Mechanics, vol. 670, pp. 518\u2013605, 2011.<\/p>\n[2] G. Araya, C. Lagares, and K. Jansen, \u201cDirect simulation of a Mach-5 turbulent spatially developing boundary layer,\u201d 49th AIAA Fluid Dynamics Conference, AIAA AVIATION Forum, (AIAA-2019-3340) 17 &#8211; 21 June, Dallas, TX, 2019.<\/p>\n[3] G. Araya, C. Lagares, and K. Jansen, \u201cReynolds number dependency in supersonic spatially-developing turbulent boundary layers,\u201d 2020 AIAA SciTech Forum (AIAA-2020-0574) 6 &#8211; 10 January, Orlando, FL., 2020.<\/p>\n[4] G. Araya and K. Jansen, \u201cEffects of wall curvature on hypersonic turbulent spatially-developing boundary layers,\u201d 2020 AFOSR\/ONR\/HVSI Hypersonic Aerodynamics Portfolios Review. DOI: 10.13140\/RG.2.2.27763.66081, 2020.<\/p>\n[5] G. Araya, C. Lagares, J. Santiago, and K. Jansen, \u201cWall temperature effect on hypersonic turbulent boundary layers via DNS,\u201d AIAA Scitech 2021 Forum (AIAA-2021-1745), 2021.<\/p>\n[6] J. G. Santiago and J. C. Dutton, \u201cVelocity measurements of a jet injected into a supersonic crossflow,\u201d Journal of Propulsion and Power, vol. 13, no. 2, pp. 264\u2013273, 1997.<\/p>\n[7] S. J. Beresh, J. F. Henfling, R. J. Erven, and R. W. Spillers, \u201cTurbulent characteristics of a transverse supersonic jet in a subsonic compressible crossflow,\u201d AIAA Journal, vol. 43, no. 11, pp. 2385\u20132394, 2005.<\/p>\n[8] M. Rasquin, C. Smith, K. Chitale, E. S. Seol, B. A. Matthews, J. L. Martin, O. Sahni, R. M. Loy, M. S. Shephard, and K. E. Jansen, \u201cScalable implicit flow solver for realistic wing simulations with flow control,\u201d Computing in Science &amp; Engineering, vol. 16, no. 6, pp. 13\u201321, 2014.<\/p>\n[9] A. N. Lab, \u201chttp:\/\/aurora.alcf.anl.gov,\u201d 2015.<\/p>\n[10] Lagares, Christian, and Guillermo Araya. 2023. &#8220;A GPU-Accelerated Particle Advection Methodology for 3D Lagrangian Coherent Structures in High-Speed Turbulent Boundary Layers&#8221; Energies 16, no. 12: 4800. <a href=\"https:\/\/doi.org\/10.3390\/en16124800\">https:\/\/doi.org\/10.3390\/en16124800<\/a><\/p>\n[\/et_pb_accordion_item][et_pb_accordion_item title=&#8221;Effects of wall curvature on hypersonic turbulent spatially-developing boundary layers (AFOSR#FA9550-17-1-0051)&#8221; _builder_version=&#8221;4.9.4&#8243; open=&#8221;off&#8221;]\n<p style=\"text-align: center\">Guillermo Araya<sup>1<\/sup>and Kenneth Jansen<sup>2<\/sup><\/p>\n<p style=\"text-align: center\"><sup>1<\/sup>Department of Mechanical Engineering, University of Puerto Rico at Mayagez (UPRM), PR 00681<\/p>\n<p style=\"text-align: center\"><sup>2<\/sup>Department of Aerospace Engineering Sciences, University of Colorado at Boulder (UCB), CO 80309<\/p>\n<h2><strong>Introduction<\/strong><\/h2>\n<p>Turbulent boundary layers that evolve along the flow direction are ubiquitous. Computationally speaking, this type of boundary layer poses an enormous challenge, due to the need for accurate and time-dependent inflow turbulence information. Moreover, accounting for the effects of wall-curvature driven pressure gradient and flow compressibility adds significant complexity to the problem. Consequently, hypersonic spatially-developing turbulent boundary layers (SDTBL) over curved walls are of crucial importance in aerospace applications, such as unmanned high-speed vehicles, scramjets and advanced space aircrafts. More importantly, hypersonic capabilities would provide faster responsiveness and longer range coverage to U.S. Air Force systems. Furthermore, an air transportation vehicle travelling at a Mach number of 5.1 might cover the New York-London route in roughly 75 minutes. Thus, the acquired understanding of the physics behind hypersonic boundary layers over curved wall-bounded flows can lead to the development of more efficient control techniques for the fluid flow (e.g., wave drag reduction) and aerodynamic heating on hypersonic vehicle design. In this sense, state-of-the-art numerical simulations performed at the petascale level will be able to supply rich and valuable information.<\/p>\n<p>&nbsp;<\/p>\n<h2><strong>Intellectual Merit <\/strong><\/h2>\n<p>We seek to develop a robust turbulent inflow generation methodology for hypersonic SDTBL (Mach numbers up to 5) in a suite of high spatial\/temporal resolution Direct Numerical Simulation (DNS) as well as Large Eddy Simulation (LES) at higher Reynolds numbers. The prescription of realistic inflow turbulent conditions is used to evaluate the downstream influence of convex (favorable pressure gradient) and concave (adverse pressure gradient) wall curvatures on: (i) low\/high order statistics of ow parameters (velocity, density, pressure and temperature), (ii) intermittency, (iii) energy budget, (iv) power spectra of velocity\/temperature fluctuations, and (v) the strong Reynolds analogy (SRA) relations. Furthermore, the extensive information supplied by DNS allows us: (i) to assess the impact of wall-curvature driven pressure gradients on the large-scale structures, and (ii) to propose improvements to sub-grid scale (SGS) turbulence models for the LES approach. The proposed open-source finite-element flow solver (PHASTA) has been able to simulate complex geometries and has shown a great scalability for petascale computing in more than 512,000 cores in Mira (Argonne&#8217;s 10 Petaflop Supercomputer). To our knowledge, the proposed petascale DNS\/LES study on hypersonic boundary layers on complex geometries and high Reynolds numbers is carried out for the first time.<\/p>\n<p><strong>\u00a0<\/strong><\/p>\n<h2><strong>Broader Impact<\/strong><\/h2>\n<p>The proposed petascale DNS contributes to better understanding of supersonic\/ hypersonic SDTBL under the influence of concave\/convex curvature, which can lead to the determination of appropriate flow control tools and design optimization in hypersonics science. We will do the highest possible and practical Reynolds number for DNS to compare to Wall Resolved LES. Then we will push the Wall Resolved LES up to higher Reynolds numbers, similar to experimental ones from the literature. Since most of the studies on the role of wall curvature-driven pressure gradients in hypersonic boundary layers have focused only on the velocity field, the proposed numerical experiments will be used to enhance the understanding of the thermal field, as well. Therefore, the uniqueness of this work lies in strengthening the fundamental knowledge of the thermal transport on supersonic\/hypersonic curved wall-bounded flows.<\/p>\n<p style=\"text-align: center\"><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Concave_convex_LESmesh.png\" alt=\"\" class=\"wp-image-451 alignnone size-full\" style=\"margin-left: auto;margin-right: auto\" width=\"500\" height=\"346\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Concave_convex_LESmesh.png 982w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Concave_convex_LESmesh-300x208.png 300w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Concave_convex_LESmesh-768x532.png 768w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Concave_convex_LESmesh-160x111.png 160w\" sizes=\"auto, (max-width: 500px) 100vw, 500px\" \/><\/p>\n<p style=\"text-align: center\">Schematic of the finite-element hybrid mesh (hexahedrals and prisms) for DNS (flow from left to right)<\/p>\n<p style=\"text-align: center\">\n<p style=\"text-align: center\"><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/QCriterion_UFluct.png\" alt=\"\" class=\"wp-image-452 alignnone size-full\" width=\"6900\" height=\"2200\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/QCriterion_UFluct.png 6900w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/QCriterion_UFluct-300x96.png 300w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/QCriterion_UFluct-1024x326.png 1024w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/QCriterion_UFluct-768x245.png 768w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/QCriterion_UFluct-160x51.png 160w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/QCriterion_UFluct-1536x490.png 1536w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/QCriterion_UFluct-2048x653.png 2048w\" sizes=\"auto, (max-width: 6900px) 100vw, 6900px\" \/>Iso-surfaces of Q-criterion colored by instantaneous streamwise velocity fluctuations, <em>u<\/em>&#8216;.<\/p>\n<p style=\"text-align: center\"><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/U_Ufluct_crop.png\" alt=\"\" class=\"wp-image-453 alignnone size-full\" width=\"4096\" height=\"1230\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/U_Ufluct_crop.png 4096w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/U_Ufluct_crop-300x90.png 300w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/U_Ufluct_crop-1024x308.png 1024w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/U_Ufluct_crop-768x231.png 768w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/U_Ufluct_crop-160x48.png 160w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/U_Ufluct_crop-1536x461.png 1536w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/U_Ufluct_crop-2048x615.png 2048w\" sizes=\"auto, (max-width: 4096px) 100vw, 4096px\" \/>Instantaneous streamwise velocity colored by streamwise velocity fluctuations, <em>u<\/em>&#8216;.<\/p>\n<p style=\"text-align: center\"><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Umag_TKE_2.png\" alt=\"\" class=\"wp-image-454 alignnone size-full\" width=\"7680\" height=\"4320\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Umag_TKE_2.png 7680w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Umag_TKE_2-300x169.png 300w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Umag_TKE_2-1024x576.png 1024w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Umag_TKE_2-768x432.png 768w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Umag_TKE_2-160x90.png 160w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Umag_TKE_2-1536x864.png 1536w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2021\/06\/Umag_TKE_2-2048x1152.png 2048w\" sizes=\"auto, (max-width: 7680px) 100vw, 7680px\" \/>Instantaneous velocity magnitude colored by turbulent kinetic energy.<\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" class=\"alignnone size-full wp-image-182\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-20-at-8.57.45-AM.png\" alt=\"\" width=\"810\" height=\"373\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-20-at-8.57.45-AM.png 2750w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-20-at-8.57.45-AM-300x138.png 300w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-20-at-8.57.45-AM-1024x471.png 1024w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-20-at-8.57.45-AM-768x354.png 768w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-20-at-8.57.45-AM-160x74.png 160w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-20-at-8.57.45-AM-1536x707.png 1536w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-20-at-8.57.45-AM-2048x943.png 2048w\" sizes=\"auto, (max-width: 810px) 100vw, 810px\" \/><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" class=\"aligncenter wp-image-149 size-full\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig1_2.png\" alt=\"\" width=\"974\" height=\"550\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig1_2.png 974w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig1_2-300x169.png 300w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig1_2-768x434.png 768w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig1_2-160x90.png 160w\" sizes=\"auto, (max-width: 974px) 100vw, 974px\" \/><\/p>\n<p>&nbsp;<\/p>\n[\/et_pb_accordion_item][et_pb_accordion_item title=&#8221;High-end visualization of coherent structures and turbulent events in wall-bounded flows with a passive scalar (NSF-GECAT #074984-16663)&#8221; _builder_version=&#8221;3.0.47&#8243; open=&#8221;off&#8221;]\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: center\">Guillermo Araya<sup>1<\/sup>, Guillermo Marin<sup>2<\/sup>&amp; Fernando Cucchietti<sup>2<\/sup><\/p>\n<p style=\"text-align: center\"><sup>1<\/sup>Dept. of Mechanical Eng., University of Puerto Rico at Mayaguez, PR 00681, USA.<\/p>\n<p style=\"text-align: center\"><sup>2<\/sup>Barcelona Supercomputing Center, Barcelona 08034, Spain.<\/p>\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<p>This project leverages the participants&#8217; expertise in the area of Direct Numerical Simulation (DNS), thermal-fluids, parallel programming, scientific visualization and virtual reality to identify, assess, track and visualize coherent structures and turbulent events in pressure-gradient boundary layers and their implication in passive scalar transport. Time-dependent 3D flow visualization involves dealing with massive amounts of data, which implies huge computational resources, not to mention a previous Navier-Stokes equation solving. The main research objectives are three-fold: (i) to perform DNS of spatially-developing turbulent boundary layers subject to streamwise pressure gradients with passive scalar transport, (ii) to conduct post-processing interface software development in order to make DNS data readable by Autodesk Maya, Blender, Paraview and Unity-3D game engine, and (iii) to carry out scientific visualization of turbulent structures and events by means of flow animations and fully immersive approach or virtual reality (VR). For such endeavor, the role of the Barcelona Supercomputing Center (BSC) will be crucial in terms of availability of cutting-edge technology (for instance, Mare Nostrum supercomputer and Visualization Group) as well as expertise of its personnel.<\/p>\n<p><strong>Intellectual Merit<\/strong>: These research efforts are making use of tremendous computational resources, not only during the running stage, but also in the visualization-animation stage. Therefore, state-of-the-art parallel computing and graphics processing unit (GPU) programming are essential. Furthermore, the high spatial\/temporal resolution of DNS will shed important light on the physics behind turbulent events and passive scalar transport in highly accelerated\/decelerated boundary layers for potential applications to flow\/heat transfer control and turbulence modeling.<\/p>\n<p><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" class=\"aligncenter wp-image-150 size-full\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_1.png\" alt=\"\" width=\"772\" height=\"375\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_1.png 772w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_1-300x146.png 300w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_1-768x373.png 768w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_1-160x78.png 160w\" sizes=\"auto, (max-width: 772px) 100vw, 772px\" \/><\/p>\n<p style=\"text-align: center\">Iso-surfaces of ejections (<strong>Q2<\/strong>) and sweeps (<strong>Q4<\/strong>) in highly accelerated boundary layers.<\/p>\n<p><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" class=\"wp-image-151 size-full aligncenter\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_2.png\" alt=\"\" width=\"974\" height=\"568\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_2.png 974w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_2-300x175.png 300w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_2-768x448.png 768w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_2-160x93.png 160w\" sizes=\"auto, (max-width: 974px) 100vw, 974px\" \/><\/p>\n<p><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" class=\"aligncenter wp-image-152 size-full\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_3.png\" alt=\"\" width=\"974\" height=\"527\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_3.png 974w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_3-300x162.png 300w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_3-768x416.png 768w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig2_3-160x87.png 160w\" sizes=\"auto, (max-width: 974px) 100vw, 974px\" \/><\/p>\n<p>&nbsp;<\/p>\n[\/et_pb_accordion_item][et_pb_accordion_item title=&#8221;Turbulence modeling and coherent structure assessment in crossflow jets (NASA PR Space Grant Fellowships)&#8221; _builder_version=&#8221;3.0.47&#8243; open=&#8221;off&#8221;]\n<p>&nbsp;<\/p>\n<p style=\"text-align: center\">German G. Saltar<sup>1<\/sup>, Carlos Quinones<sup>1<\/sup>, Walter Silva<sup>2<\/sup>&amp; Guillermo Araya<sup>1<\/sup><\/p>\n<p style=\"text-align: center\"><sup>1<\/sup>Dept. of Mechanical Eng., University of Puerto Rico at Mayaguez, PR 00681, USA.<\/p>\n<p style=\"text-align: center\"><sup>2<\/sup>NASA Langley Research Center, Hampton, VA 23681, USA.<\/p>\n<p>&nbsp;<\/p>\n<p>Incompressible jets transversely issuing into a spatially-developing turbulent boundary layer is one of the most challenging types of three dimensional flows due to its thermal-fluid complexity and technological applications; for instance, film cooling of turbine blades, fuel or dilution air injection in gas turbine engines, thrust vector control, chimney plumes, just to name a few. The ability to control a flow field in such a way to enhance thermal efficiency is of crucial relevance in aerospace and other engineering applications. Direct Numerical Simulation (DNS) with high spatial and temporal resolution of jets in crossflow subject to very strong Favorable Pressure Gradient (FPG) has been successfully performed during 2017-2018, as part of the NASA PR Space Grant project entitled \u201cDNS of crossflow jets subject to very strong favorable pressure gradient\u201d by Mr. C. Quinones (graduate student) and Dr. Araya (advisor). The analysis was done by prescribing accurate turbulent information (instantaneous velocity and temperature) at the inlet of a computational domain for simulations of spatially-developing turbulent boundary layers. The major achievements and dissemination were: one MSc thesis proposal, three oral presentations, one peer-reviewed conference proceedings article, and, two journal papers in progress. The large and extensive DNS dataset generated (of approximately1.5TB in size) will be postprocessed and analyzed for turbulence modeling purposes and for the objective study of turbulent coherent structures, i.e. Lagrangian Coherent Structures (LCS). The main research objectives of the proposed continuation project are two-fold. The first goal involves performing Reynolds-averaged Navier-Stokes (RANS) simulations of spatially-developing turbulent boundary layers subject to the combined effect of a crossflow jet at different velocity ratios (VR = 0.5 and 1) and streamwise favorable pressure gradient with passive scalar transport. The second goal consists on a better understanding of the physics behind momentum\/scalar Lagrangian coherent motions emanating from crossflow jets.<\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" class=\"alignnone size-full wp-image-155\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig-3_1.png\" alt=\"\" width=\"1450\" height=\"540\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig-3_1.png 1450w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig-3_1-300x112.png 300w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig-3_1-1024x381.png 1024w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig-3_1-768x286.png 768w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Fig-3_1-160x60.png 160w\" sizes=\"auto, (max-width: 1450px) 100vw, 1450px\" \/><\/p>\n[\/et_pb_accordion_item][et_pb_accordion_item title=&#8221;Turbulence modelling for aerospace applications (XSEDE #CTS170006)&#8221; _builder_version=&#8221;3.0.47&#8243; open=&#8221;off&#8221;]\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<p>Computational Fluid Dynamics (CFD) is significantly gaining ground in the area of aerospace research due to its relative low cost, high accuracy and versatility. Particularly during the design stage of an airplane, it is possible to obtain fast results of different configurations, and, thus minimize the time and the expense of building a wind tunnel model and testing it. Furthermore, with the recent advent of petascale supercomputers with hundreds of thousands of cores, the running time of large scale systems, such as a complete airplane, has been dramatically reduced.<\/p>\n<p><img loading=\"lazy\" loading=\"lazy\" decoding=\"async\" class=\"alignnone size-full wp-image-179\" src=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-17-at-6.07.04-PM.png\" alt=\"\" width=\"2154\" height=\"1140\" srcset=\"https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-17-at-6.07.04-PM.png 2154w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-17-at-6.07.04-PM-300x159.png 300w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-17-at-6.07.04-PM-1024x542.png 1024w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-17-at-6.07.04-PM-768x406.png 768w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-17-at-6.07.04-PM-160x85.png 160w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-17-at-6.07.04-PM-1536x813.png 1536w, https:\/\/ceid.utsa.edu\/garaya\/wp-content\/uploads\/sites\/121\/2018\/09\/Screen-Shot-2018-09-17-at-6.07.04-PM-2048x1084.png 2048w\" sizes=\"auto, (max-width: 2154px) 100vw, 2154px\" \/><\/p>\n<p>&nbsp;<\/p>\n[\/et_pb_accordion_item][\/et_pb_accordion][\/et_pb_column][\/et_pb_row][\/et_pb_section]\n","protected":false},"excerpt":{"rendered":"<p>[et_pb_section fb_built=&#8221;1&#8243; admin_label=&#8221;Section&#8221; _builder_version=&#8221;3.22&#8243;][et_pb_row admin_label=&#8221;Row&#8221; _builder_version=&#8221;3.25&#8243; background_size=&#8221;initial&#8221; background_position=&#8221;top_left&#8221; background_repeat=&#8221;repeat&#8221;][et_pb_column type=&#8221;4_4&#8243; _builder_version=&#8221;3.25&#8243; custom_padding=&#8221;|||&#8221; custom_padding__hover=&#8221;|||&#8221;][et_pb_text admin_label=&#8221;Text&#8221; _builder_version=&#8221;4.9.7&#8243; header_text_color=&#8221;#000000&#8243; background_size=&#8221;initial&#8221; background_position=&#8221;top_left&#8221; background_repeat=&#8221;repeat&#8221; text_orientation=&#8221;center&#8221; module_alignment=&#8221;center&#8221; use_border_color=&#8221;off&#8221; border_color=&#8221;#ffffff&#8221; border_style=&#8221;solid&#8221;] Flow Animation and Research Projects Scientific visualization of high spatial\/temporal resolution numerical simulations (i.e. DNS or LES) is carried out. In addition, mixed reality (MR) has been implemented by the development [&hellip;]<\/p>\n","protected":false},"author":241,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_et_pb_use_builder":"on","_et_pb_old_content":"","_et_gb_content_width":"","_monsterinsights_skip_tracking":false,"_monsterinsights_sitenote_active":false,"_monsterinsights_sitenote_note":"","_monsterinsights_sitenote_category":0,"footnotes":""},"class_list":["post-578","page","type-page","status-publish","hentry"],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v27.3 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>Research - Guillermo Araya<\/title>\n<meta name=\"robots\" content=\"index, follow, max-snippet:-1, max-image-preview:large, max-video-preview:-1\" \/>\n<link rel=\"canonical\" href=\"https:\/\/ceid.utsa.edu\/garaya\/research\/\" \/>\n<meta property=\"og:locale\" content=\"en_US\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"Research - Guillermo Araya\" \/>\n<meta property=\"og:description\" content=\"[et_pb_section fb_built=&#8221;1&#8243; admin_label=&#8221;Section&#8221; _builder_version=&#8221;3.22&#8243;][et_pb_row admin_label=&#8221;Row&#8221; _builder_version=&#8221;3.25&#8243; background_size=&#8221;initial&#8221; background_position=&#8221;top_left&#8221; background_repeat=&#8221;repeat&#8221;][et_pb_column type=&#8221;4_4&#8243; _builder_version=&#8221;3.25&#8243; custom_padding=&#8221;|||&#8221; custom_padding__hover=&#8221;|||&#8221;][et_pb_text admin_label=&#8221;Text&#8221; _builder_version=&#8221;4.9.7&#8243; header_text_color=&#8221;#000000&#8243; background_size=&#8221;initial&#8221; background_position=&#8221;top_left&#8221; background_repeat=&#8221;repeat&#8221; text_orientation=&#8221;center&#8221; module_alignment=&#8221;center&#8221; use_border_color=&#8221;off&#8221; border_color=&#8221;#ffffff&#8221; border_style=&#8221;solid&#8221;] Flow Animation and Research Projects Scientific visualization of high spatial\/temporal resolution numerical simulations (i.e. DNS or LES) is carried out. 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