Application of low drag-due-to-lift concept of linearized theory to the studies of twist and camber of isolated wing and wing-body configurations of supersonic aircraft
SUPERSONIC AERODYNAMIC CHARACTERISTICS OF SOME SIMPLIFIED AND COMPLEX AIRCRAFT CONFIGURATIONS WHICH EMPLOY HIGHLY SWEPT TWISTED-AND-CAMBERED ARROW-WING PLANFORMS
1963-01-01
Conference paper
No indication
English
Aerodynamic Characteristics of Canard-Forward Swept Wing Aircraft Configurations
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