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 | 15 | 2019 |
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 | 10 | 2021 |
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 | 9 | 2021 |
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 | 6 | 2019 |
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 | 5 | 2022 |
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 | 5 | 2022 |
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 | 5 | 2020 |
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 | 4 | 2023 |
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 | 1 | 2024 |
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 |