NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Improvements to Wall Corrections at the NASA Langley 14 x 22-Ft Subsonic TunnelThe new wall pressure measurement system and the TWICS wall correction system for the 14x22-Ft subsonic tunnel are described. Results from a recent semispan test and a full-span test are presented. Comparison with existing classical methods of correction is shown. A modification of the TWICS code to treat the effect due to a deflected wake from a high-lift wing is also discussed. The current implementation of TWICS for the 14x22-Ft tunnel is shown to be an improvement over existing methods.
Document ID
20030098032
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Iyer, Venkit (Lockheed Martin Corp. United States)
Kuhl, David D. (Lockheed Martin Corp. United States)
Walker, Eric L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA Paper 2003-3950
Report Number: AIAA Paper 2003-3950
Meeting Information
Meeting: 21st AIAA Applied Aerodynamics Conference
Location: Orlando, FL
Country: United States
Start Date: June 23, 2003
End Date: June 26, 2003
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available