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The Influence of the Application of Power during Spin Recovery of Multiengine AirplanesThe effect of application of power, so far not clarified, is investigated in the present report in order to give the pilot, in addition to the control measures, an expedient for spin recovery of multiengine airplanes. To this end, a series of spins was performed with an airplane of the Go 150 type. It was possible to set up a uniform rule regarding the effect of power, for right end left spins as well as for any combination of the direction of rotation of the propellers.
Document ID
20050029434
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Hoehler, P. (Zentrale fuer Wissenschaftliches Berichtswesen Berlin, Germany)
Date Acquired
August 22, 2013
Publication Date
June 1, 1949
Publication Information
Publication: ZWB Forschungsbericht Nr. 1536
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-TM-1219
Report Number: NACA-TM-1219
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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