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Computation of supersonic flow over flying configurations
Title:
Computation of supersonic flow over flying configurations
Author:
Năstase, Adriana.
ISBN:
9780080449579
9780080556994
Personal Author:
Edition:
1st ed.
Publication Information:
Amsterdam : Elsevier, 2008.
Physical Description:
1 online resource (xvii, 389 pages) : illustrations
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.
Abstract:
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 results show the real world application of computational results * Easy computation and visualization of inviscid and viscous aerodynamis characteristics of flying configerations * Includes a fully optimized and integrated design for a proposed supersonic transport aircraft.
Genre:
Electronic Access:
ScienceDirect http://www.sciencedirect.com/science/book/9780080449579Available:*
Shelf Number | Item Barcode | Shelf Location | Status |
|---|---|---|---|
| TL571 .N37 2008 EB | 1189044-1001 | Elsevier E-Book Collections | Searching... |
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