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Computation of Supersonic Flow over Flying Configurations

Computation of Supersonic Flow over Flying Configurations - Nastase, Adriana - ISBN: 9780080449579
Prijs: € 193,75 (onder voorbehoud)
Beschikbaarheid: Titel is niet in voorraad. Levertijd onbekend.
Bindwijze: Boek, Gebonden (20-12-2007)
Genre: Luchtvaart- en ruimtetechniek
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Beschrijving

The book presents new reinforced, zonal, and spectral solutions for the boundary value problems of the PDE of compressible 3-dimensional stationary Navier-Stokes layer of the flow over flattened flying configurations (FC). These solutions are especially well suited for optimal design of economical and ecologically viable integrated STA and space vehicles, optimal design of recuperation of reusable satellites and recuperation of reusable boosters of vertically launched space vehicles.

Details

Titel: Computation of Supersonic Flow over Flying Configurations
auteur: Nastase, Adriana
Mediatype: Boek
Bindwijze: Gebonden
Taal: Engels
Aantal pagina's: 410
Uitgever: Elsevier Science
Plaats van publicatie: 03
Publicatiedatum: 2007-12-20
NUR: Luchtvaart- en ruimtetechniek
Afmetingen: 240 x 165
ISBN/ISBN13: 0080449573
ISBN/ISBN13: 9780080449579
Intern nummer: 6745331

Inhoudsopgave

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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