Effects of Leading-edge Slats on the Aerodynamic Characteristics of a 45 Degree Sweepback Wing-fuselage Configuration at Mach Numbers of 0.4 to 1.03
1953-08-21
Miscellaneous
No indication
English
Curvature and Leading-Edge Sweepback Effects on Grid Fin Aerodynamic Characteristics
British Library Conference Proceedings | 1993
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