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Experimental Flights for Testing of a Reactor as an Expedient for the Termination of Dangerous SpinsIn the Institute for Flight Mechanics of the DVL a reactor arrangement with a maximum output of 100 kg was investigated as an expedient for the termination of dangerous spins on an airplane of the FW 56 type. reproduce the influence of a disturbance of the steady spin condition by a pitching or yawing moment. The tests were meant to reproduce the influence of a disturbance of the steady spin condition by a pitching and yawing moment.
Document ID
20050242932
Acquisition Source
Headquarters
Document Type
Other - NACA Technical Memorandum
Authors
Hoehler, P.
(Zentrale fuer Wissenschaftliches Berichtswesen Berlin, Germany)
Koeppen, I. v.
(Zentrale fuer Wissenschaftliches Berichtswesen Berlin, Germany)
Date Acquired
August 23, 2013
Publication Date
July 1, 1949
Publication Information
Publication: Zentrale fuer Wissenschaftliches Berichtswesen bei der Deutschen Versuchsanstalt fuer Luftfahrt Nr. 1027
Subject Category
Aerodynamics
Report/Patent Number
NACA-TM-1221
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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