A reduced order aerothermodynamic modeling framework for hypersonic vehicles based on surrogate and POD-Reference-Cited by-同舟云学术

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A reduced order aerothermodynamic modeling framework for hypersonic vehicles based on surrogate and POD

Published:2015-10 Issue:5 Volume:28 Page:1328-1342
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Chen Xin,Liu Li,Long Teng,Yue Zhenjiang

Funder

National Natural Science Foundation of China

Beijing Institute of Technology of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference33 articles.

1. Cazier Jr FW, Ricketts RH. Structural dynamic and aeroelastic considerations for hypersonic vehicles. Reston: AIAA; 1991. Report No.: AIAA-1991-1255.

2. Fidan B, Mirmirani M, Ionnou P. Flight dynamics and control of air-breathing hypersonic vehicles: review and new directions. Reston: AIAA; 2003. Report No.: AIAA-2003-7081.

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

4. Studies on fluid-thermal-structural coupling for aerothermoelasticity in hypersonic flow;Culler;AIAA J,2010

5. Application of integrated fluid-thermal-structure analysis methods;Weiting;Thin-walled Struct,1991

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