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A Simulator Study of T-tail Aircraft in Deep Stall ConditionsFixed base simulation study of T-tail aircraft deep stall and recovery
Document ID
19660020099
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lina, L. J.
(NASA Langley Research Center Hampton, VA, United States)
Moul, M. T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-56806
Accession Number
66N29389
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
RECOVERY
T TAIL SURFACE
AIRCRAFT PERFORMANCE
SIMULATION
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