Numerical simulation of sonic boom near-field flow over C25D model

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 Simula...

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Hauptverfasser: Kiseleva, T. A., Lukashevich, S. V.
Format: Tagungsbericht
Sprache:eng
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Zusammenfassung: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.
ISSN:0094-243X
1551-7616
DOI:10.1063/5.0052077