Transformation of Perturbations in Supersonic Gas Flow Subject to Oblique Shock Wave

Transformation of Perturbations in Supersonic Gas Flow Subject to Oblique Shock Wave

In a supersonic flow, disturbances of different parameters arise. These perturbations can have a significant impact on the interaction of the flow with the surface. When gas flow passes through a shock wave, perturbations are transformed depending on the initial parameters of the flow. Therefore, it...

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Bibliographic Details
Main Authors: Andriy A. Avramenko, Igor V. Shevchuk, Margarita M. Kovetskaya, Yulia Y. Kovetska, Andrii I. Tyrinov, Dmytro V. Anastasiev
Format: Article
Language:English
Published: MDPI AG 2025-04-01
Series:Aerospace
Subjects:
supersonic flow
shock wave
turbulent flow
heat transfer
instability
Online Access:https://www.mdpi.com/2226-4310/12/4/323
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