Concept of maneuver margin is discussed, and definitions are suggested which are applicable to all types of configurations; calculations are presented for maneuver characteristics of simplified flexible models representing conventional and slender integrated aircraft.
Static aeroelastic deformation of slender configurations -- 4. Manoeuvre theory
Aeronautical Quarterly
Aeronautical Quarterly ; 14 , Part 4
1963
20 pages
Aufsatz (Zeitschrift)
Englisch
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British Library Conference Proceedings | 2010
|Some static aeroelastic considerations of slender aircraft
Engineering Index Backfile | 1961
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