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Static and dynamic longitudinal stability derivatives of a powered 0.18-scale model of a fan-in-wing VTOL aircraftStatic and dynamic longitudinal stability tests of fan in wing V/STOL aircraft model
Document ID
19680006425
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Chambers, J. R.
(NASA Langley Research Center Hampton, VA, United States)
Grafton, S. B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1968
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-4322
Report Number: NASA-TN-D-4322
Accession Number
68N15894
Funding Number(s)
CONTRACT_GRANT: 721-01-00-26-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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