Effect of thermal protection system size on aerothermoelastic stability of the hypersonic panel-Reference-Cited by-同舟云学术

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Effect of thermal protection system size on aerothermoelastic stability of the hypersonic panel

Published:2020-11 Issue: Volume:106 Page:106170
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Xie Dan,Dong Bin,Jing Xingjian

Funder

Chinese NSF

Shaanxi NSF

Hong Kong Scholar

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

1. Airbreathing hypersonic propulsion at Pratt & Whitney-overview;Kazmar,2005

2. Coupled flow, thermal, and structural analysis of aerodynamically heated panels;Thornton;J. Aircr.,1988

3. Aeroelastic and aerothermoelastic analysis in hypersonic flow: past, present, and future;McNamara;AIAA J.,2011

4. Verification tests of durable thermal protection system concepts;Shideler;J. Spacecr. Rockets,1985

5. Parametric weight comparison of advanced metallic, ceramic tile, and ceramic blanket thermal protection systems;Myers,2000

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1. Vibration Characteristics and Aeroelastic Stability Behavior of Foam-Filled Composite Corrugated Sandwich Panels Considering Mass Reduction;Journal of Aerospace Engineering;2024-03

2. Effect of surface radiation on the surface heat flux of two-dimensional hypersonic panel flow;Physics of Fluids;2023-03-01

3. Spectral Proper Orthogonal Decomposition Reduced-Order Model for Analysis of Aerothermoelasticity;AIAA Journal;2023-02

4. Thermo-mechanical performance of 3D-printed TC4 hierarchical lattice-truss-core sandwich structures in high temperature conditions;Mechanics of Advanced Materials and Structures;2022-05-11

5. Thermo-mechanical analysis of a multilayer hollow cylindrical thermal protection structure with functionally graded ultrahigh-temperature ceramic to be heat resistant layer;Aerospace Science and Technology;2022-05

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