Computation of Supersonic Flow over Flying Configurations

Author:   Adriana Nastase (Aerodynamik des Fluges, University of Technology RWTH, Aachen, Germany)
Publisher:   Elsevier Science & Technology
ISBN:  

9780080449579


Pages:   410
Publication Date:   20 December 2007
Format:   Hardback
Availability:   Awaiting stock   Availability explained
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Computation of Supersonic Flow over Flying Configurations


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Author:   Adriana Nastase (Aerodynamik des Fluges, University of Technology RWTH, Aachen, Germany)
Publisher:   Elsevier Science & Technology
Imprint:   Elsevier Science Ltd
Dimensions:   Width: 16.50cm , Height: 2.80cm , Length: 24.00cm
Weight:   0.870kg
ISBN:  

9780080449579


ISBN 10:   0080449573
Pages:   410
Publication Date:   20 December 2007
Audience:   Professional and scholarly ,  Professional & Vocational
Format:   Hardback
Publisher's Status:   Active
Availability:   Awaiting stock   Availability explained
The supplier is currently out of stock of this item. It will be ordered for you and placed on backorder. Once it does come back in stock, we will ship it out for you.

Table of 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

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