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Spin tests of a single-engine, high-wing light airplaneThe airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high velocity. The airplane recovers almost immediately after any deviation from the prospin control positions, except for one maneuver with reduced flexibility in the elevator control system.
Document ID
19820008195
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Stewart, E. C. (NASA Langley Research Center Hampton, VA, United States)
Suit, W. T. (NASA Langley Research Center Hampton, VA, United States)
Moul, T. M. (NASA Langley Research Center Hampton, VA, United States)
Brown, P. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TP-1927
L-14305
Report Number: NASA-TP-1927
Report Number: L-14305
Accession Number
82N16068
Funding Number(s)
PROJECT: RTOP 505-41-13-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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