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Large-scale wind-tunnel tests on an aspect ratio 2.17 delta-wing model equipped with midchord boundary-layer-control flapsWind tunnel tests on aspect ratio 2.17 delta wing model with midchord boundary layer control flaps
Document ID
19650002305
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Corsiglia, V. R. (NASA Ames Research Center Moffett Field, CA, United States)
Koenig, D. G. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1964
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2552
Report Number: NASA-TN-D-2552
Accession Number
65N11906
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
BOUNDARY LAYER CONTROL
WIND TUNNEL
ASPECT RATIO

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