Panel-Flutter Analysis of a Thermal Protection-Shield Concept for the Space Shuttle
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference7 articles.
1. Stochastic properties of turbulence excited rotor blade vibrations
2. Structural Fatigue under Non-Stationary Random Loading
3. Interpolation of aerodynamic damping of lifting rotors in forward flight from measured response variance
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1. Combined thermal phenomena of hypersonic vehicle;SCIENTIA SINICA Physica, Mechanica & Astronomica;2019-09-16
2. Aeroelastic Stability of Thermal Protection System for Inflatable Aerodynamic Decelerator;Journal of Spacecraft and Rockets;2015-01
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