Effect of Vertical-Tail Area and Length on Yawing Stability Characteristics of Model Having 45° Sweptback Wing.
Effect of vertical-tail area and length on yawing stability characteristics of model having 45° sweptback wing
NACA -- Tech Note
1951
49 pages
Illus, Diagrs, Charts, Tables
Report
English
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Engineering Index Backfile | 1952
|Engineering Index Backfile | 1950
|Engineering Index Backfile | 1943
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