In present paper, Royal Aircraft Establishment test results have been analyzed and are applied to American designs; simpler design criterion, based solely on type and dimensions of tail, has been developed; it is useful in rapid estimation of whether new design is likely to comply with minimum requirements for safety in spinning.
Approximate spin design criterion for monoplanes
Nat Advisory Committee Aeronautics -- Tech Note
1939
7 pages
4 Supp sheets, Bibliography
Report
English
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An approximate spin design criterion for monoplanes
TIBKAT | 1940
|An approximate spin design criterion for monoplanes
SLUB | 1939
|Emerald Group Publishing | 1941
Engineering Index Backfile | 1941
Engineering Index Backfile | 1920
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