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Use of a pitot probe for determining wing section drag in flightA wake traversing probe was used to obtain section drag and wake profile data from the wing of a sailplane. The transducer sensed total pressure defect in the wake as well as freestream total pressure on both sides of the sensing element when the probe moved beyond the wake. Profiles of wake total pressure defects plotted as a function of distance above and below the trailing edge plane were averaged for calculating section drag coefficients for flights at low dynamic pressures.
Document ID
19760003922
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Saltzman, E. J.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: Kansas Univ. Proc. of the NASA, Ind., Univ., Gen. Aviation Drag Reduction Workshop
Subject Category
Aircraft Instrumentation
Accession Number
76N11010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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