Computation of Supersonic Flow over Flying Configurations

Computation of Supersonic Flow over Flying Configurations is a high-level aerospace reference book that 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 resultsEasy computation and visualization of inviscid and viscous aerodynamic characteristics of flying configurationsIncludes a fully optimized and integrated design for a proposed supersonic transport aircraft

Chapter 1. Zonal, Spectral Solutions for the Three-Dimensional, Compressible Navier-Stokes Layer
Chapter 2. Hyperbolic Potential Boundary Value Problems of the Axial Disturbance Velocities of Outer Flow, at NSL's Edge
Chapter 3. Computation of Axial Disturbance 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
Chapter 5. The Aerodynamic Characteristics of Flying Configurations with Arbitrary Shapes, in Supersonic Flow
Chapter 6. The Visualization of the Surfaces of Pressure Coefficients and Aerodynamic Characteristics of Wedged Delta and Rectangular Wings, in Supersonic Flow
Chapter 7. Qualitative Analysis of the NSL's Asymptotical 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 Aerodynamical Global Optimal Design
Chapter 10. Comparison of the Theoretical Aerodynamic Characteristics of Wing Models with Experimental Determined Results
Final Remarks
Book Presentation
Outlook
Subject Index
Author Index