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Aerodynamic characteristics of a five jet VTOL configuration in the transition speed rangeWind tunnel tests of a VTOL jet fighter to determine aerodynamic characteristics including stability
Document ID
19680026609
Acquisition Source
Legacy CDMS
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
October 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4812
Report Number: NASA-TN-D-4812
Accession Number
68N36081
Funding Number(s)
CONTRACT_GRANT: 721-01-00-18-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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