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Resonant Triad in Boundary-Layer Stability: Composite Solution and Comparison with Observations - Part 2Here, numerical results are computed from an asymptotic near-resonance triad analysis. The analysis considers a resonant triad of instability waves consisting of a plane fundamental wave and a pair of symmetrical oblique subharmonic waves. The relevant scaling ensures that nonlinearity is confined to a distinct critical layer. The analysis is first used to form a composite solution that accounts for both the flow divergence and nonlinear effects. It is shown that the backreaction on the plane Tollmien Schlichting (TS) fundamental wave, although fully accounted for, is of little significance. The observed enhancement at the fundamental frequency disturbance is not in the plane TS wave, but is caused by nonlinearly generated waves at the fundamental frequency that result from nonlinear interactions in the critical layer. The saturation of the oblique waves is caused by their self-interaction. The nonlinear phase-locking phenomenon, the location of resonance with respect to the neutral stability curve, low frequency effects, detuning in the streamwise wave numbers, and nonlinear distortion of the mode shapes are discussed. Nonlinearity modifies the initially two dimensional Blasius profile into a fuller one with spanwise periodicity. The interactions at a wide range of unstable spanwise wave numbers are considered, and the existence of a preferred spanwise wave number is explained by means of the vorticity distribution in the critical layer. Besides presenting novel features of the phenomena and explaining the delicate mechanisms of the interactions, the results of the theory are in excellent agreement with experimental and numerical observations for all stages of the development and for various input parameters.
Document ID
19910023145
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mankbadi, Reda R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1991
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-105209
E-6045-1
NAS 1.15:105209
Report Number: NASA-TM-105209
Report Number: E-6045-1
Report Number: NAS 1.15:105209
Accession Number
91N32459
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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