Computation of Supersonic Flow over Flying Configurations
- 1st Edition - February 16, 2014
- Author: Adriana Nastase
- Language: English
- Hardback ISBN:9 7 8 - 0 - 0 8 - 0 4 4 9 5 7 - 9
- Paperback ISBN:9 7 8 - 0 - 0 8 - 0 9 7 5 0 4 - 7
- eBook ISBN:9 7 8 - 0 - 0 8 - 0 5 5 6 9 9 - 4
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… Read more
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 results
- Easy computation and visualization of inviscid and viscous aerodynamic characteristics of flying configurations
- Includes a fully optimized and integrated design for a proposed supersonic transport aircraft
University libraries and departmental/institute libraries, space centres such as NASA, DLR, DGLR, ONERA, FOI, ESA etc. American Institute of Physics; Association Francaise de Mechanique; Corporate aerospace companies such as Boeing, Airbus etc.
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
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
- Edition: 1
- Published: February 16, 2014
- Language: English
AN
Adriana Nastase
Affiliations and expertise
Aerodynamik des Fluges, University of Technology RWTH, Aachen, GermanyRead Computation of Supersonic Flow over Flying Configurations on ScienceDirect