Aerodynamic Characteristics of a Three-Engine Supersonic Transport Model Having a Low- Aspect-Ratio Variable-Sweep Warped Wing
1964
61 pages
Report
No indication
English
Aircraft , Fluid Mechanics , Aerodynamic characteristics , Low aspect ratio wing , Supersonic transport , Variable sweep , Aerodynamic , Camber , Characteristics , Coefficient , Dihedral , Edge , Engine , Lateral , Leading , Lift , Longitudinal , Low aspect , Model , Nacelle , Ratio , Stability , Supersonic , Sweep , Tail , Three , Transport , Variable , Vertical , Warp , Wing