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Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft modelWind tunnel investigation of steady state aerodynamics of composite lift VTOL aircraft model combining rotary and fixed wings
Document ID
19690018719
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Huston, R. J. (NASA Langley Research Center Hampton, VA, United States)
Winston, M. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1969
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-5232
Report Number: NASA-TN-D-5232
Accession Number
69N28097
Funding Number(s)
CONTRACT_GRANT: 721-01-00-36-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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