Buch, Englisch, 410 Seiten, Format (B × H): 168 mm x 241 mm, Gewicht: 862 g
Buch, Englisch, 410 Seiten, Format (B × H): 168 mm x 241 mm, Gewicht: 862 g
ISBN: 978-0-08-044957-9
Verlag: Elsevier Science
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.
Zielgruppe
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.
Autoren/Hrsg.
Fachgebiete
Weitere Infos & Material
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
