Hypersonic fluid–thermal–structural interaction of cone–slice–ramp: computations with experimental validation
The paper presents an investigation of fluid–thermal–structural interaction (FTSI) on a
complex geometry in hypersonic flows. The objective is to assess high-fidelity numerical …
complex geometry in hypersonic flows. The objective is to assess high-fidelity numerical …
Fluid–structural coupling of an impinging shock–turbulent boundary layer interaction at Mach 3 over a flexible panel
J Hoy, I Bermejo-Moreno - Flow, 2022 - cambridge.org
We present high-fidelity numerical simulations of the interaction of an oblique shock
impinging on the turbulent boundary layer developed over a rectangular flexible panel …
impinging on the turbulent boundary layer developed over a rectangular flexible panel …
Fluid–Thermal–Structure Interaction of Hypersonic Inlets Under Different Aspect Ratios
WY Su, H An, MY Wang - AIAA Journal, 2023 - arc.aiaa.org
It is crucial to consider the fluid–thermal–structural interaction (FTSI) in designing the
scramjet inlet for sustained hypersonic flight. To understand the aerothermal and aeroelastic …
scramjet inlet for sustained hypersonic flight. To understand the aerothermal and aeroelastic …
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… - AIAA SciTech 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0291. vid The paper presents an
investigation of fluid-thermal-structural interaction (FTSI) on a complex geometry in …
investigation of fluid-thermal-structural interaction (FTSI) on a complex geometry in …
Maximizing Lift-to-Drag and Thrust-to-Drag Ratios for Trimmed Hypersonic Vehicles
CC Mbagwu, DJ Dalle, JF Driscoll - Journal of Aircraft, 2023 - arc.aiaa.org
Ways to maximize the lift-to-drag (L/D) and the thrust-to-drag (T/D) ratios of hypersonic
vehicles are computed using the reduced-order model Michigan-AFRL Scramjet in Vehicle …
vehicles are computed using the reduced-order model Michigan-AFRL Scramjet in Vehicle …
Applications of Gaussian Process Regression in the Aero-Thermo-Servo-Elastic Analysis Towards Integrated Hypersonic Flight Dynamic Analysis
D Huang - 2021 60th IEEE Conference on Decision and …, 2021 - ieeexplore.ieee.org
This tutorial paper presents the surrogate modeling based on Gaussian process regression
(GPR) and its application in the hypersonic aero-thermo-servo-elastic analysis, a key …
(GPR) and its application in the hypersonic aero-thermo-servo-elastic analysis, a key …
High-Speed Fluid-Structure Interactions on a Compliant Panel
BAL Vasconcelos, P Eduardo - 2023 - unsworks.unsw.edu.au
This work investigates first-of-kind experiments to measure fluid-structure interactions (FSI)
on a clamped-free-clamped-free compliant panel at Mach 5.8 in a Ludwieg tube. The panel …
on a clamped-free-clamped-free compliant panel at Mach 5.8 in a Ludwieg tube. The panel …
[图书][B] Monolithic multiphysics simulation of hypersonic aerothermoelasticity using a hybridized discontinuous Galerkin method
WP England - 2023 - search.proquest.com
This work presents implementation of a hybridized discontinuous Galerkin (DG) method for
robust simulation of the hypersonic aerothermoelastic multiphysics system. Simulation of …
robust simulation of the hypersonic aerothermoelastic multiphysics system. Simulation of …
[PDF][PDF] Joint Experimental/Computational Study of Fluid-Thermal-Structural Interaction of a Cone-Slice-Ramp in Hypersonic Flow.
A Pandey - 2021 - osti.gov
Air-breathing hypersonic vehicles endure intense aerothermodynamic loading. As a
consequence, the vehicle's structural characteristics and desired performance change …
consequence, the vehicle's structural characteristics and desired performance change …