Publication Date:
2019-06-28
Description:
An averaging total pressure wake rake used by the Cessna Aircraft Company in flight tests of a modified 210 airplane with a laminar flow wing was calibrated in wind tunnel tests against a five-tube pressure probe. The model generating the wake was a full-scale model of the Cessna airplane wing. Indications of drag trends were the same for both instruments.
Keywords:
AERODYNAMICS
Type:
NASA-CR-181630
,
NAS 1.26:181630
,
AR-87-1
Format:
application/pdf
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