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Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight testsAerodynamic factors, and effects on dynamic longitudinal stability characteristics of tilt wing V/STOL aircraft
Document ID
19680006472
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-4344
Report Number: NASA-TN-D-4344
Accession Number
68N15941
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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