Work

Numerical simulation of the interaction between weak shock waves and supersonic boundary layer on a flat plate with the blunt leading edge

Year: 2024

Type: article

Abstract: The interaction of weak shock waves in form of an N-wave with the supersonic laminar boundary layer on a flat plate with blunt leading edge at the free-stream Mach number M = 2.5 is numerically studied. The numerical results are compared with known experimental data. The combined influence of the N-wave and the leading edge bluntness on the laminar-turbulent transition process is discussed.

Source: Fluid Dynamics

DOI: 10.31857/s1024708424020102

Authors: I. V. Egorov, N. K. Nguen, P. V. Chuvakhov

Institutions: Moscow Institute of Physics and Technology, Central Aerohydrodynamic Institute

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: bronze

OpenAlex ID: W4403565425

FWCI:

Cites: 6

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Related to: 10