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A study to determine effects of applying thrust on recovery from incipient and developed spins for four airplane configurationsEffects of applying thrust along with optimum aerodynamic control surface defections on incipient and developed spin-recovery characteristics of four aircraft configurations
Document ID
19660019276
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Grafton, S. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1966
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3416
Accession Number
66N28566
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC STABILITY
CONTROL SURFACE
THRUST EFFECT
AIRCRAFT CONFIGURATION

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