NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effect of sidewall suction on flow in two-dimensional wind tunnelsA closed-form analysis of flow in a two-dimensional subsonic wind tunnel that uses sidewall suction around the model to reduce sidewall boundary-layer effects is presented. The model problem that is treated involves a flat plate airfoil in a tunnel with a suction window shaped to permit an analytic solution. This solution shows that the lift coefficient depends explicitly on the porosity parameter of the suction window and implicitly on the suction pressure differential. For a given sidewall displacement thickness, the lift coefficient increases as the suction-window porosity decreases.
Document ID
19930039541
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Barnwell, Richard W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: AIAA Journal
Volume: 31
Issue: 1
ISSN: 0001-1452
Subject Category
Aerodynamics
Accession Number
93A23538
Distribution Limits
Public
Copyright
Other

Available Downloads

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