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COMPUTATION OF SUPERSONIC FLOW OVER FLYING CONFIGURATIONS
Computation of Supersonic Flow over Flying Configurations
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By
Adriana Nastase, Aerodynamik des Fluges, University of Technology RWTH, Aachen, Germany

Audience
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.

Contents
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

Bibliographic details
Hardbound, 410 pages, publication date: DEC-2007
ISBN-13: 978-0-08-044957-9
ISBN-10: 0-08-044957-3
Imprint: ELSEVIER

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GBP 120.99
EUR 142.95
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Last update: 5 Sep 2009
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