Work

The effect of weak shock waves on the flow in the boundary layer of a plate when the - sweep angle changes

Year: 2025

Type: article

Source: Thermophysics and Aeromechanics

DOI: 10.1134/s0869864325010044

Authors: L. V. Afanasev, Yu. G Ermolaev, A. D. Kosinov, N. V. Semenov, B. V. Smorodsky, A. S. Shmakov, A. A. Yatskikh

Institution: Institute of Theoretical and Applied Mechanics

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4416569711

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Cites: 10

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