A new force-measuring balance for large-scale model in hypersonic wind tunnel
Author:
Affiliation:
1. School of Mechanical Engineering, SouthWest Jiaotong University, Chengdu 610031, People’s Republic of China
2. China Aerodynamics Research and Development Center, Mianyang, Sichuan 621000, China
Funder
National Natural Science Foundation of China
Fundamental Research Funds for the Central Universities
Publisher
AIP Publishing
Subject
Instrumentation
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0054090
Reference15 articles.
1. R. W. Guy, C. R. Rogers, R. L. Puster, K. E. Rock, and G. S. Diskin, “The NASA Langley scramjet test complex,” AIAA Paper 96-3243, 1996.
2. Design of a pulse-type strain gauge balance for a long-test-duration hypersonic shock tunnel
3. Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel
4. A new dynamic modelling methodology of a force measuring system for hypersonic impulse wind tunnel
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