NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effects Of Compressibility On Dynamic StallReport presents results of computations and measurements of compressible flow about an airfoil, angle of attack of which oscillates about static-stall angle. Study focuses on effects of compressibility on dynamic stall. Of particular interest are conditions determining onset of separation of flow, which leads to premature dynamic stall and consequent significant reduction of lift.
Document ID
19920000315
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Carr, L. W.
(NASA Ames Research Center, Moffett Field, CA.)
Fung, K.-Y.
(Arizona Univ.)
Date Acquired
August 15, 2013
Publication Date
May 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 5
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-12473
Accession Number
92B10315
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

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