Coupled Flow-Thermal-Structural Analysis for Response Prediction of Hypersonic Vehicle Skin Panels

Author:

Culler Adam,McNamara Jack

Publisher

American Institute of Aeronautics and Astronautics

Cited by 17 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Coupling Strategies for Analyzing Fluid-Thermal-Structural Interactions of a Hypersonic Inlet;AIAA SCITECH 2024 Forum;2024-01-04

2. Numerical investigation of the influence of aerothermoelastic dynamic response on the performance of the three-dimensional hypersonic inlet;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-03-03

3. A Fast Calculation and Rendering Method for Infrared Characteristics of Hypersonic Vehicle;Journal of Physics: Conference Series;2020-07-01

4. Model Updating and Uncertainty Propagation in Aerothermoelastic Analysis for C/SiC Panel of Ceramic Matrix Composite;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02

5. Robust Aeroelastic Design Optimization of Hypersonic Vehicle with Uncertainties in Aerodynamic Loads, Heat Flux, and Structure;58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2017-01-05

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