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:   Out of stock   Availability explained
The supplier is temporarily out of stock of this item. It will be ordered for you on backorder and shipped when it becomes available.

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Computation of Supersonic Flow over Flying Configurations


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Overview

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.

Full Product Details

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:   Out of stock   Availability explained
The supplier is temporarily out of stock of this item. It will be ordered for you on backorder and shipped when it becomes available.

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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