Modal Characteristics of Carbon Fiber Reinforced Composite Structure at High Temperature-Reference-Cited by-同舟云学术

Modal Characteristics of Carbon Fiber Reinforced Composite Structure at High Temperature

Published:2021-01 Issue:1 Volume:58 Page:182-189
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Zhengping Zhang¹,Hao Cheng¹,Fang Ren¹,Zhenqiang Wu¹,Haibo Li¹,Fanjin Kong¹

Affiliation:

1. Beijing Institute of Structure and Environment Engineering, 100076 Beijing, People’s Republic of China

Funder

Key Laboratory Foundation

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Reference24 articles.

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2. Thermoacoustic loads and fatigue of hypersonic vehicle skin panels

3. TzongG.JacobsR.LiguoreS. “Air Vehicle Integration and Technology Research (AVIATR) Task Order 0015: Predictive Capability for Hypersonic Structural Response and Life Prediction, Phase 1–Identification of Knowledge Gaps, Volume 1–Nonproprietary Version,” U.S. Air Force Research Lab. TR AFRL-RB-WP-TR-2010-3068, V1, Wright–Patterson AFB, OH, 2010.

4. Effects of Radiation Heating on Modal Characteristics of Panel Structures

5. VosteenL. F.McWitheyR. R.ThomsonR. G. “Effect of Transient Heating on Vibration Frequencies of Some Simple Wing Structures,” NACA TN-4054, 1957.

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