Elementary description of aerodynamics of problem of regaining and maintaining control after engine failure; three situations considered are: sudden failure of engine; steady flight under asymmetric power; balked landing with one or more engines dead.
Control in flight under asymmetric power
Aircraft Eng
Aircraft Engineering ; 19 , n 223 ; p 287-290
1947
4 pages
Aufsatz (Zeitschrift)
Englisch
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Control in Flight Under Asymmetric Power
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