Stability and Control Characteristics of Complete Airplane Model Having Wing with Quarter-Chord Line Swept Back 40°, Aspect Ratio 2.50, and Taper Ratio 0.42.
Stability and control characteristics of complete airplane model having wing with quarter-chord line swept back 40°, aspect ratio 2.50, and taper ratio 0.42
NACA -- Tech Note
1951
86 pages
Illus, Diagrs, Charts, Tables
Report
English
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