Tabulated Data from a Pressure-Distribution Investigation at Mach Number 2.01 of the Wing of a Canard Airplane Model
1959
201 pages
Report
No indication
English
Aerodynamics , Fluid Mechanics , Aircraft model , Pressure distribution , Table , Trapezoidal wing , Aircraft , Angle of attack , Coefficient , Deflection , Distribution , Forebody , Geometry , Model , Position , Pressure , Supersonic , Tail , Test , Trapezoidal , Tunnel , Vertical , Wing