Longitudinal Stability, Control Effectiveness, and Drag Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Configuration Having an Unswept Tapered Wing of Aspect Ratio 3.0 and NACA 65A004.5 Airfoil Sections
Author : John C. Jr McFall
Publisher :
Page : 30 pages
File Size : 16,39 MB
Release : 1953
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ISBN :