Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations
1978
76 S
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Close-coupled canard-wing vortex interaction
AIAA | 1984
|Effect of Canard Deflection on Close-Coupled Canard-Wing-Body Aerodynamics
Online Contents | 1994
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