Force measurements in hypersonic impulse facilities
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Cited by 13 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Stress-wave balance for measuring the aerodynamic drag force in impulse hypersonic facilities;Shock Waves;2021-11-30
2. An accelerometer balance for aerodynamic force measurements over Hypervelocity Ballistic models in shock tunnel;Measurement;2019-03
3. Transient Dynamics Research on the Force-Measurement System for Hypersonic Impulse Combustion Wind Tunnel Based on Inertia Compensation;Journal of Aerospace Engineering;2018-11
4. Finite Element Analysis of the Unsteady Thrust Characteristics of Pulse Detonation Engines;Journal of Engineering for Gas Turbines and Power;2016-07-06
5. Unsteady Drag Measurements for Hypersonic Shock Tunnel;29th International Symposium on Shock Waves 1;2015
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