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Large-scale wind tunnel investigation of a ducted fan - Deflected-slipstream model with an auxiliary wingWind tunnel investigation of longitudinal aerodynamic characteristics of semispan wing deflected-slipstream configuration with double slotted flap and auxiliary wing
Document ID
19710014385
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Falarski, M. D. (Army Air Mobility Research and Development Lab. Moffett Field, CA, United States)
Mort, K. W. (Army Air Mobility Research and Development Lab. Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-6323
A-3670
Report Number: NASA-TN-D-6323
Report Number: A-3670
Accession Number
71N23861
Funding Number(s)
CONTRACT_GRANT: 721-01-11-02-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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