NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A thin-layer solution of the flow about a prolate spheroidComputational results are presented for the transitional or turbulent flow about a prolate spheroid, at alpha = 10 deg or 30 deg, correspondingly, using an implicit, approximately factored, partially flux-split algorithm, based on the thin-layer equations. The computed flow field is in good agreement with available experimental data.
Document ID
19880062519
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Panaras, A. G.
(NASA Ames Research Center Moffett Field, CA, United States)
Steger, J. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1988
Publication Information
Publication: Zeitschrift fuer Flugwissenschaften und Weltraumforschung
Volume: 12
ISSN: 0342-068X
Subject Category
Aerodynamics
Accession Number
88A49746
Distribution Limits
Public
Copyright
Other

Available Downloads

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