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LARGE-SCALE WIND-TUNNEL TESTS IN GROUND EFFECT OF A 35 DEG SWEPTBACK WING JET TRANSPORT MODEL EQUIPPED WITH BLOWING BOUNDARY-LAYER-CONTROL TRAILING- AND LEADING-EDGE FLAPSWind tunnel test of ground effect of 35-deg swept- back wing jet transport equipped with boundary layer control, trailing & leading edge flaps
Document ID
19630006046
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Aoyagi, K. (NASA Ames Research Center Moffett Field, CA, United States)
Hickey, D. H. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1963
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TN-D-1884
Report Number: NASA-TN-D-1884
Accession Number
63N15922
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL STABILITY TEST
TRAILING-EDGE FLAP
JET TRANSPORT
SWEPTBACK WING
BOUNDARY LAYER CONTROL

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