Publication Date:
2019-07-13
Description:
A novel laser-based sensor for the in situ measurement of wind tunnel model angle of attack is described and the results of a successful demonstration in the NASA Ames 9 x 7-ft. Supersonic wind tunnel are presented. The design concepts of a scanning laser-based turbulence detector, which will enable nonintrusive, microscopic studies of the onset and extent of transition on wind tunnel test models, is also described.
Keywords:
INSTRUMENTATION AND PHOTOGRAPHY
Type:
International Instrumentation Symposium; May 03, 1987 - May 08, 1987; Las Vegas, NV; United States
Format:
text
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