6 1/2 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
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
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