Fully Coupled Nonlinear Aerothermoelastic Computational Model of a Plate in Hypersonic Flow
Author:
Affiliation:
1. Technion–Israel Institute of Technology, Haifa, Israel 3200003
2. Duke University, Durham, NC 27708
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060085
Reference20 articles.
1. Hypersonic and High-Temperature Gas Dynamics, Second Edition
2. Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future
3. Reduced-Order Aerothermoelastic Framework for Hypersonic Vehicle Control Simulation
4. Enhanced Modal Solutions for Structural Dynamics in Aerothermoelastic Analysis
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