This high level aerospace reference book will be useful for undergraduate, and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows. * Computational work and experimental results show the real world application of computational results* Easy computation and visualization of inviscid and viscous aerodynamis characteristics of flying configerations* Includes a fully optimized and integrated design for a proposed supersonic transport aircraft

Chapter 1. Zonal, Spectral Solutions for the Three-Dimensional, Compressible Navier-Stokes LayerChapter 2. Hyperbolic Potential Boundary Value Problems of the Axial Disturbance Velocities of Outer Flow, at NSL's EdgeChapter 3. Computation of Axial Disturbance Velocities on Wedged Wings, in Supersonic Flow, at NSL's EdgeChapter 4. Computation of Axial Disturbance Velocities on Flying Configurations with Arbitrary Shapes, in Supersonic Flow, at NSL's EdgeChapter 5. The Aerodynamic Characteristics of Flying Configurations with Arbitrary Shapes, in Supersonic FlowChapter 6. The Visualization of the Surfaces of Pressure Coefficients and Aerodynamic Characteristics of Wedged Delta and Rectangular Wings, in Supersonic FlowChapter 7. Qualitative Analysis of the NSL's Asymptotical Behaviours in the Vicinity of its Critical ZonesChapter 8. Computation of the Friction Drag Coefficients of the Flying ConfigurationsChapter 9. Inviscid and Viscous Aerodynamical Global Optimal DesignChapter 10. Comparison of the Theoretical Aerodynamic Characteristics of Wing Models with Experimental Determined ResultsFinal RemarksBook PresentationOutlookSubject IndexAuthor Index