Effect of Pressure Gradient on Local Excitation of Boundary-layer Instability Due to Free-stream Turbulence and Micro Surface Roughness

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Shen L.; Lu C.

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Journal Paper

Paper Information

Journal: JOURNAL OF APPLIED FLUID MECHANICS (JAFM) Year:2021 | Volume:14 | Issue:4 Page(s): 1103-1111

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Title

Effect of Pressure Gradient on Local Excitation of Boundary-layer Instability Due to Free-stream Turbulence and Micro Surface Roughness

Author(s)

Shen L. | Lu C. | Issue Writer Certificate

Keywords

Pressure gradientQ4

ReceptivityQ4

Boundary LayerQ4

Roughness elementQ4

Abstract

The prediction and control of the laminar-turbulent transition is crucial to the designs of vehicles, turbines, etc. The initial condition of transition depends on the exciting process of boundary-layer instability, which is the key to implement its prediction and control. The current researches confirm that the exciting process of boundary-layer instability, namely Receptivity, is affected not only by different types of free-stream disturbances and shape parameters of surface Roughness elements, but also by the Pressure gradient of mean flow. Hence, we study the effect of pressure-gradient on local excitation of boundary-layer instability under the interaction of the low-level, isotropic free-stream turbulence and micro surface roughness in this work. The numerical results reveal the pressure-gradient effect on the receptive process and the group speed of excited wave packets in the Falkner-Skan Boundary Layer. The favorable/adverse Pressure gradients (FPG/APG) are found to be able to promote/suppress the excitation and subsequent evolution of Tollmien–Schlichting (T-S) waves. Then the relations of the Pressure gradient with the amplitude, growth rate, wave number, phase speed and shape function of excited T-S waves are studied.

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