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Numerical experiments in boundary-layer stabilityNumerical solution of the three-dimensional incompressible Navier-Stokes equations is used to study the instability of a flat-plate boundary layer in a manner analogous to the vibrating-ribbon experiments. Flow-field structures are observed which are very similar to those found in the vibrating-ribbon experiment to which computational initial conditions have been matched. Streamwise periodicity is assumed in the simulation so that the evolution occurs in time, but the events which constitute the instability are so similar to the spatially occurring ones of the laboratory that it seems clear the physical processes involved are the same. A spectral and finite difference numerical algorithm is employed in the simulation.
Document ID
19800039787
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wray, A.
(NASA Ames Research Center Moffett Field, CA, United States)
Hussaini, M. Y.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 80-0275
Report Number: AIAA PAPER 80-0275
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Pasadena, CA
Start Date: January 14, 1980
End Date: January 16, 1980
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
80A23957
Distribution Limits
Public
Copyright
Other

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