The new wall pressure measurement system and the TWICS wall correction system for the 14x22-Ft subsonic tunnel are described. Results from a recent semi-span 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.
Improvements to Wall Corrections at the NASA Langley 14X22 Foot Subsonic Tunnel
2003
20 pages
Report
Keine Angabe
Englisch
AIAA-2003-3950 Improvements to Wall Corrections at the NASA Langley 14x22-Ft Subsonic Tunnel
British Library Conference Proceedings | 2003
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