The Upper-Branch Stability of Compressible Boundary Layer Flows

The Upper-Branch Stability of Compressible Boundary Layer Flows
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
Total Pages: 38
Release: 2018-10-15
Genre: Science
ISBN: 9781728745589

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The upper-branch linear and nonlinear stability of compressible boundary layer flows is studied using the approach of Smith and Bodonyi (1982) for a similar incompressible problem. Both pressure gradient boundary layers and Blasius flow are considered with and without heat transfer, and the neutral eigenrelations incorporating compressibility effects are obtained explicitly. The compressible nonlinear viscous critical layer equations are derived and solved numerically and the results indicate some solutions with positive phase shift across the critical layer. Various limiting cases are investigated including the case of much larger disturbance amplitudes and this indicates the structure for the strongly nonlinear critical layer of the Benney-Bergeon (1969) type. It is also shown how a match with the inviscid neutral inflexional modes arising from the generalized inflexion point criterion, is achieved. Gajjar, J. S. B. and Cole, J. W. Glenn Research Center RTOP 505-62-21

Stability Analysis of the Compressible, Adiabatic Similar Boundary Layer Equations (Lower Branch).

Stability Analysis of the Compressible, Adiabatic Similar Boundary Layer Equations (Lower Branch).
Author:
Publisher:
Total Pages: 0
Release: 1983
Genre:
ISBN:

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In a previous report the authors analyzed the stability of the lower branch solutions of the incompressible (M sub infinity = O) Falkner-Skan boundary layers. There a perturbation analysis to these boundary layers was performed resulting in the Rayleigh stability equation. Eigen value solutions were obtained for the Rayleigh equation for different adverse pressure gradient (beta) values. All retarded flows were found to be unstable for a small range of frequencies with the amplification factor increasing as the extent of reversed flow increased. In this report they have entended that work by including the effect of Mach number M sub infinity on the stability of adiabatic (S sub W = O) Falker-Skan equations for beta = -.04, -.08, -.12, -.16 and -.19884. We found out that in all these cases as the Mach number M sub infinity increases the instability of flow decreases. In most of the cases the instability almost completely disappeared at M sub infinity = 3.

Boundary-layer Stability Theory

Boundary-layer Stability Theory
Author: Leslie M. Mack
Publisher:
Total Pages: 406
Release: 1969
Genre: Boundary layer
ISBN:

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