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Roughness-induced generation of crossflow vortices in three-dimensional boundary layersThe receptivity theory of Goldstein and Ruban is extended within the nonasymptotic (quasi-parallel) framework of Zavol'skii et al to predict the roughness-induced generation of stationary and nonstationary instability waves in three-dimensional, incompressible boundary layers. The influence of acoustic-wave orientation, as well as that of different types of roughness geometries, including isolated roughness elements, periodic arrays, and two-dimensional lattices of compact roughness shapes, as well as random, but spatially homogeneous roughness distributions, is examined. The parametric study for the Falkner-Skan-Cooke family of boundary layers supports our earlier conjecture that the initial amplitudes of roughness-induced stationary vortices are likely to be significantly larger than the amplitudes of similarly induced nonstationary vortices in the presence of acoustic disturbances in the free stream. Maximum unsteady receptivity occurs when the acoustic velocity fluctuation is aligned with the wavenumber vector of the unsteady vortex mode. On the other hand, roughness arrays that are oriented somewhere close to the group velocity direction are likely to produce higher instability amplitudes. Limitations of the nonasymptotic theory are discussed, and future work is suggested.
Document ID
19930017907
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Choudhari, Meelan
(High Technology Corp. Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:4505
NASA-CR-4505
Accession Number
93N27096
Funding Number(s)
CONTRACT_GRANT: NAS1-19299
PROJECT: RTOP 537-03-23-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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