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Stability and control characteristics of a large scale deflected slipsteam STOL model with a wing of 5.7 aspect ratioWind tunnel tests of stability and control characteristics of large scale model representative of propeller-driven STOL transport aircraft
Document ID
19710026959
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Page, V. R. (NASA Ames Research Center Moffett Field, CA, United States)
Aiken, T. N. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1971
Subject Category
Aircraft
Report/Patent Number
A-3342
NASA-TN-D-6393
Accession Number
71N36435
Funding Number(s)
PROJECT: RTOP 721-01-00-16-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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