Airplane tail surface design that would make recoveries from spins satisfactory was investigated in analysis of characteristics of models of approximately 100 military airplanes; relative distribution of mass along wings and fuselage, relative density of airplane, and design of vertical surfaces, considered.
Tail-design requirements for satisfactory spin recovery
Nat Advisory Committee Aeronautics -- Tech Note
1946
8 pages
Supp sheets, Bibliography
Report
Englisch
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Tail-design requirements for satisfactory spin recovery
NTRS | 1946
|Requirements for satisfactory flying qualities
Engineering Index Backfile | 1949
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