NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Numerical simulation of vortex unsteadiness on a slender body at high incidenceNumerical results obtained with the present3D thin-layer Navier-Stokes solver are shown to qualitatively follow experimental results. They also indicate the existence of at least two main frequencies on an ogive cylinder at 40 and 60 deg angles-of-attack: (1) a low frequency associated with fluctuations of the primary vortices, and leads to vortex shedding, and (2) a high frequency associated with shear-layer fluctuations that are concentrated in several small areas above the leeward side of the body's cylindrical portion.
Document ID
19920045438
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Degani, David
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 15, 2013
Publication Date
March 1, 1992
Publication Information
Publication: AIAA Journal
Volume: 30
ISSN: 0001-1452
Subject Category
Aerodynamics
Accession Number
92A28062
Distribution Limits
Public
Copyright
Other

Available Downloads

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