Transient Dynamics Research on the Force-Measurement System for Hypersonic Impulse Combustion Wind Tunnel Based on Inertia Compensation-Reference-Cited by-同舟云学术

Transient Dynamics Research on the Force-Measurement System for Hypersonic Impulse Combustion Wind Tunnel Based on Inertia Compensation

Published:2018-11 Issue:6 Volume:31 Page:04018094
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Lv Jinzhou¹,Zhang Xiaoqing²,Chen Guangxiong³,Wu Yingchuan⁴

Affiliation:

1. Lecturer, Tribology Research Institute, School of Mechanical Engineering, Southwest Jiaotong Univ., Chengdu, Sichuan 610031, China (corresponding author).

2. Research Associate, Science and Technology on Scramjet Laboratory, Hypervelocity Aerodynamics Institute, Chinese Aerodynamic Research and Development Center, Mianyang, Sichuan 621000, China.

3. Professor, Tribology Research Institute, School of Mechanical Engineering, Southwest Jiaotong Univ., Chengdu, Sichuan 610031, China.

4. Researcher, Science and Technology on Scramjet Laboratory, Hypervelocity Aerodynamics Institute, Chinese Aerodynamic Research and Development Center, Mianyang, Sichuan 621000, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000914

Reference29 articles.

1. Collopy A. X. S. Lee and E. C. Marineau. 2014. “Development of dynamic force measurement capabilities at AEDC Tunnel 9.” In Proc. 52nd AIAA Aerospace Sciences Meeting. National Harbor MD: AIAA.

2. Structural damping determination by finite element approach

3. Accelerometer-Based Force Balance for High Enthalpy Facilities

4. Image-based force and moment measurement in hypersonic facilities

5. An improved visualization-based force-measurement technique for short-duration hypersonic facilities

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