Computation of supersonic flow over flying configurations /

This high level aerospace reference book 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...

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Bibliographic Details
Call Number:Libro Electrónico
Main Author: N�astase, Adriana
Format: Electronic eBook
Language:Inglés
Published: Amsterdam : Elsevier, 2008.
Edition:1st ed.
Subjects:
Aerodynamics, Supersonic.
A�erodynamique supersonique.
Aerodynamics, Supersonic
Online Access:Texto completo
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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