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Spin-Tunnel Investigation of A 1/40-Scale Model of the F-111A Airplane with Store Loadings and with Supplementary Spin-Recovery DevicesAn investigation has been made in the Langley spin tunnel to determine the spin and spin-recovery characteristics of the F-111A airplane in the symmetric and asymmetric stores loading conditions. Tests were also made with the model in the clean condition to determine whether the spin-recovery characteristics could be improved by the use of supplementary devices.
Document ID
20000021277
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Bowman, James S., Jr. (NASA Langley Research Center Hampton, VA United States)
White, William L. (NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1974
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-SX-2970
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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