The Spinning of Model Aircraft and the Prediction of Full-scale Spin Recovery Characteristics PDF Download
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Author: Aeronautical Research Council (Great Britain)
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 104
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Book Description
Author: Aeronautical Research Council (Great Britain)
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 104
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Book Description
Author: G. E. Pringle
Publisher:
ISBN:
Category :
Languages : en
Pages : 193
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Book Description
Author: G. E. Pringle
Publisher:
ISBN:
Category :
Languages : en
Pages : 104
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Book Description
Author: William D. Grantham
Publisher:
ISBN:
Category : Spin (Aerodynamics)
Languages : en
Pages : 52
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Book Description
Author: James S. Bowman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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Book Description
A summary was made of all NASA (and NACA) research and experience related to the spin and recovery characteristics of light personal-owner-type general-aviation airplanes. Very little of the research deals with light general-aviation airplanes as such, but many of the airplanes and models tested before and during World War II were similar to present-day light general-aviation airplanes with regard to the factors that are important in spinning. The material is based mainly on the results of spin-tunnel tests of free-spinning dynamically scaled models of about 100 different airplane designs and, whenever possible, includes correlation with full-scale spin tests. The research results are discussed in terms of airplane design considerations and the proper use of controls for recovery.
Author: T. H. Kerr
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 19
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Author: Aeronautical Research Council
Publisher:
ISBN:
Category : Spin (Aerodynamics)
Languages : en
Pages : 14
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Author: Harry E. Murray
Publisher:
ISBN:
Category : Laplace transformation
Languages : en
Pages : 744
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Book Description
The lateral motions of aircraft are obtained by means of the Laplace transform which gives solutions in terms of elementary functions for the free motions and the motions due to forcing step functions. The lateral stability of a specific airplane and certain of its free and forced motions are calculated.
Author: Oscar Seidman
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
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Book Description
Summary: Because large airplanes of the transport and bomber categories have been reported to have spun inadvertently, the available information on the subject has been reviewed. Results of model tests, as well as reports of full-scale-airplane spins, were considered. It is concluded that large airplanes should not be intentionally spun because these aircraft are not designed for the loads and speeds that may be encountered in the spin and recovery. If a large airplane is stalled, wither inadvertently or for familiarization purposes, the pilot should apply sufficient down elevator to relieve the stall at the very first sign of stalling. The throttles should be closed if the airplane has started to roll off into a turn and the nose has dropped appreciably. Even after the airplane has rolled off on a wing, the pilot can regain control by promptly moving the stick forward and then using all three controls to return t level flight.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1154
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Book Description
