Computation of Supersonic Flow over Flying Configurations

6 ½ X 9 7/16 in Chapter 1. Zonal, Spectral Solutions for the Three-Dimensional, Compres sible Navier-Stokes Layer Chapter 2. Hyperbolic Potential Boundary Value Problems of the Axial Disturbance Velocities of Outer Flo w, at NSL’s Edge Chapter 3. Computation of Axial Disturban ce Velocities on Wedged Wings, in Supersonic Flow, at NSL’s Edge Chapter 4. Computation of Axial Disturbance Velocities on Flying Configurations with Arbitrary Shapes, in Supersonic Flow, at NSL’s Edge< BR id=‘CRLF’>Chapter 5. The Aerodynamic Characteristics of Flying Confi gurations with Arbitrary Shapes, in Supersonic Flow Chapter 6. The Visualization of the Surfaces of Pressure Coefficients and Aero dynamic Characteristics of Wedged Delta and Rectangular Wings, in Supers onic Flow Chapter 7. Qualitative Analysis of the NSL’s Asy mptotical Behaviours in the Vicinity of its Critical Zones
Chapter 8. Computation of the Friction Drag Coefficients of the Flying Configurations Chapter 9. Inviscid and Viscous Aerodynamic al Global Optimal Design Chapter 10. Comparison of the Theo