Static Aerodynamic Characteristics of a Model of a Typical Subsonic Jet-Transport Airplane at Mach Numbers from 0.40 to 1.20
1967
41 pages
Report
No indication
English
Fluid Mechanics , Jet transport , Static aerodynamic characteristics , Subsonic aircraft , Aerodynamic , Aerodynamics , Aircraft , Angle of attack , Characteristics , Coefficient , Dihedral , Jet , Lift , Mach number , Model , Pressure , Stability , Static , Subsonic , Sweep , Transport , Wing