CRITERION FOR THE LAMINAR-TURBULENT TRANSITION ONSET IN A COMPRESSIBLE BOUNDARY LAYER

A criterion of the laminar-turbulent transition onset in a compressible boundary-layer flow is formulated on the base of Liepmann’ assumption according to which the critical condition is reached where the Reynolds stress (caused by the laminar oscillations) becomes equal to the shear stress of the base (undisturbed) flow. Comparison with known results of direct numerical simulations of disturbances propagating in the non-gradient boundary layers on flat plates and sharp cones at zero angle of attack showed that the criterion works well in a wide range of local Mach numbers (0 < Me < 7) for different mechanisms of the nonlinear breakdown of unstable waves.

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Publication Details

Journal
Доклады Российской академии наук Физика технические науки / Doklady Physics
Published
2025-01-01
DOI
https://doi.org/10.7868/s3034508125030077
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
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article

CRITERION FOR THE LAMINAR-TURBULENT TRANSITION ONSET IN A COMPRESSIBLE BOUNDARY LAYER

Ivan V. Egorov
Доклады Российской академии наук Физика технические науки / Doklady Physics
Computational Fluid Dynamics and Aerodynamics
article

CRITERION FOR THE LAMINAR-TURBULENT TRANSITION ONSET IN A COMPRESSIBLE BOUNDARY LAYER

Ivan V. Egorov
article en

Abstract

A criterion of the laminar-turbulent transition onset in a compressible boundary-layer flow is formulated on the base of Liepmann’ assumption according to which the critical condition is reached where the Reynolds stress (caused by the laminar oscillations) becomes equal to the shear stress of the base (undisturbed) flow. Comparison with known results of direct numerical simulations of disturbances propagating in the non-gradient boundary layers on flat plates and sharp cones at zero angle of attack showed that the criterion works well in a wide range of local Mach numbers (0 < Me < 7) for different mechanisms of the nonlinear breakdown of unstable waves.

Доклады Российской академии наук Физика технические науки / Doklady PhysicsVol. 522(1)
Openalex Percentile: Top 73%
Computational Fluid Dynamics and Aerodynamics
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