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Aerodynamic Characteristics of Twin Propeller Deflected Slipstream STOL Airplane Model with Boundary Layer Control on Inverted V-tailAerodynamic characteristics of COIN aircraft model with boundary layer control on inverted V-tail
Document ID
19690001604
Document Type
Other - NASA Technical Note (TN)
Authors
Gentry, G. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Margason, R. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1968
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-4856
Accession Number
69N10935
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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