Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 5. Wing Net Chordwise Pressure Distributions and Isobars - Nacelles on, Part 2
1972
266 pages
Report
No indication
English
Aircraft , Fluid Mechanics , Aerodynamic loading , Supersonic aircraft , Aerodynamic control surfaces , Varying sweep wings , Jet transport planes , Experimental data , Graphics , Angle of attack , Mach number , Jet engine nacelles , Pressure , Load distribution , Transonic flow , Supersonic flow , Delta wings , Design , Flaps(Control surfaces) , Leading edge flaps , Trailing edge , Deflection , Data processing , Mathematical prediction , Interpolation , Sst technology follow on program , Supersonic transports