NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Application of the method of integral relations to laminar boundary layers in three dimensionsThe method of integral relations is extended to general three-dimensional compressible laminar boundary layer flows. The transformation employed to transform the basic three-dimensional compressible boundary layer equations into quasi-incompressible form is an extension of the Howarth transformation. The resulting system of differential equations is integrated numerically by the method of integral relations as proposed by Dorodnitsyn. To demonstrate the accuracy of the method, it is applied to calculation of the parabolic flow over a flat plate and the boundary flow over an infinite yawed cylinder, for which solutions are known. It is then applied to the flow over a flat plate disturbed by a cylinder normal to the plate, for which a finite-difference solution is available for comparison. It is finally applied to calculating the crossflow velocity variation for supersonic flow over a swept wedge.
Document ID
19770045820
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Holt, M.
(California Univ. Berkeley, CA, United States)
Modarress, D.
(California, University Berkeley, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
March 25, 1977
Subject Category
Aerodynamics
Accession Number
77A28672
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available