Computation of supersonic flow over flying configurations [electronic resource] / Adriana Nastase.
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...
Saved in:
| Online Access: |
Full Text (via ScienceDirect) |
|---|---|
| Main Author: | |
| Format: | Electronic eBook |
| Language: | English |
| Published: |
Amsterdam :
Elsevier,
2008.
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| Edition: | 1st ed. |
| Subjects: |
MARC
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| 100 | 1 | |a Năstase, Adriana. |0 http://id.loc.gov/authorities/names/n84800663 |1 http://isni.org/isni/0000000024172983. | |
| 245 | 1 | 0 | |a Computation of supersonic flow over flying configurations |h [electronic resource] / |c Adriana Nastase. |
| 250 | |a 1st ed. | ||
| 260 | |a Amsterdam : |b Elsevier, |c 2008. | ||
| 300 | |a 1 online resource (xvii, 389 pages) : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
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| 505 | 0 | |a 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. | |
| 504 | |a Includes bibliographical references and indexes. | ||
| 520 | |a 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. | ||
| 588 | 0 | |a Print version record. | |
| 650 | 0 | |a Aerodynamics, Supersonic. |0 http://id.loc.gov/authorities/subjects/sh85001297. | |
| 650 | 7 | |a Aerodynamics, Supersonic. |2 fast |0 (OCoLC)fst00798221. | |
| 776 | 0 | 8 | |i Print version: |a Năstase, Adriana. |t Computation of supersonic flow over flying configurations. |b 1st ed. |d Amsterdam : Elsevier, 2008 |z 9780080449579 |z 0080449573 |w (OCoLC)79447673. |
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