The results of numerical simulation of sonic boom near field flow around the NASA Concept 25D (C25D) low-boom supersonic demonstrator configuration are presented. The calculations were carried out for a stationary flow of an ideal gas in a three-dimensional mode with a help of SOLIDWORKS Flow Simulation solver. Comparison with the results of numerical simulations obtained by researchers in the framework of the 2nd AIAA Sonic Boom Prediction Workshop is made.
Numerical simulation of sonic boom near-field flow over C25D model
INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2020) ; 2020 ; Novosibirsk, Russia
AIP Conference Proceedings ; 2351 , 1
24.05.2021
5 pages
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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