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Aravinth Sadagopan
Aravinth Sadagopan
在 psu.edu 的电子邮件经过验证
标题
引用次数
引用次数
年份
A design strategy for a 6: 1 supersonic mixed-flow compressor stage
A Sadagopan, C Camci
Aerospace Science and Technology 87 (April 2019), 265-277, 2019
152019
Assessment of high-temperature effects on hypersonic aerothermoelastic analysis using multi-fidelity multi-variate surrogates
A Sadagopan, D Huang, U Duzel, LE Martin, KM Hanquist
AIAA Scitech 2021 Forum, 1610, 2021
102021
Numerical investigation of fluid-thermal-structural interaction for a control surface in hypersonic flow
A Sadagopan, D Huang, H Xu, XI Yang
AIAA Scitech 2021 Forum, 0911, 2021
92021
Viscous Flow and Performance Issues in a 6: 1 Supersonic Mixed-Flow Compressor with a Tandem Diffuser
A Sadagopan, C Camci
Aerospace Science and Technology 88 (May 2019), 9-21, 2019
62019
Study of fluid–thermal–structural interaction in high-temperature high-speed flow using multi-fidelity multi-variate surrogates
D Huang, A Sadagopan, Ü Düzel, KM Hanquist
Journal of Fluids and Structures 113, 103682, 2022
52022
An Experimental and Computational Correlation Study for Fluid-Thermal-Structural Interaction of a Control Surface in Hypersonic Flow
A Sadagopan, D Huang, A Jirasek, J Seidel, A Pandey, KM Casper
AIAA Scitech 2022 Forum, 0291, 2022
52022
Impact of high-temperature effects on the aerothermoelastic behavior of composite skin panels in hypersonic flow
A Sadagopan, D Huang, KM Hanquist
AIAA Scitech 2020 Forum, 0937, 2020
52020
Hypersonic fluid–thermal–structural interaction of cone–slice–ramp: computations with experimental validation
A Sadagopan, D Huang, A Jirasek, J Seidel, A Pandey, KM Casper
AIAA Journal 61 (11), 4752-4771, 2023
42023
Reduced-order modeling for fluid-thermal-structural interaction of cone-slice-ramp in high-speed flows
A Sadagopan, D Huang
AIAA SCITECH 2024 Forum, 1050, 2024
12024
Physical mechanism of shear layer oscillation on cone-slice-ramp in hypersonic flows
A Sadagopan, D Huang
AIAA SciTech Forum and Exposition, 2024, 2024
2024
Modal analysis of a shear layer in high-supersonic cavity flows using data-driven and operator-based resolvent analysis
A Sadagopan, D Huang, M Safari, CA Yeh
Bulletin of the American Physical Society 67, 2022
2022
A design strategy for a 6: 1 supersonic mixed-flow compressor stage and its viscous flow-based performance analysis
A Sadagopan
2019
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