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Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratiosWind tunnel determination of longitudinal force characteristics for STOL aircraft scale models with varying wing aspect ratios
Document ID
19680009302
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Deckert, W. H. (NASA Ames Research Center Moffett Field, CA, United States)
Dickinson, S. O. (NASA Ames Research Center Moffett Field, CA, United States)
Page, V. R. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1968
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-4448
Report Number: NASA-TN-D-4448
Accession Number
68N18771
Funding Number(s)
CONTRACT_GRANT: 721-01-00-16-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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