Coupled Fluid–Structural Thermal Numerical Methods for Thermal Protection System
Author:
Affiliation:
1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
2. Hubei Aerospace Technology Academy, 430040 Wuhan, People’s Republic of China
Funder
Priority Academic Program Development of Jiangsu Higher Education Institutions.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference22 articles.
1. Aerodynamic Heating of a Hypersonic Projectile with Forward-Facing Ellipsoid Cavity at Nose
2. Uncertainty dynamic theoretical analysis on ceramic thermal protection system using perturbation method
3. Aerothermal Postflight Analysis of the Sharp Edge Flight Experiment-II
4. Aeroelastic Stability of Thermal Protection System for Inflatable Aerodynamic Decelerator
5. Characterization of Complex Porous Structures for Reusable Thermal Protection Systems: Porosity Measurements
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