In this article, an improved algorithm of calculating the free-stream parameters in the test section of the hotshot wind tunnel is purposed. This algorithm accounts real gas effects and heat losses, by including experimental values of the flow velocity as a function of the gas exhaustion time. To obtain these data, we realized a two-beam time-of-flight method of velocity measurement.
Improved method of determining flow parameters in a hotshot wind tunnel
INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2016): Proceedings of the 18th International Conference on the Methods of Aerophysical Research ; 2016 ; Perm, Russia
AIP Conference Proceedings ; 1770 , 1
2016-10-13
6 pages
Conference paper
Electronic Resource
English
Hotshot Wind Tunnel Force Measurement
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