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140116s2008 enka ob 001 0 eng d |
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|a UMI
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|a 313649720
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|a 9780080556994
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|a 008055699X
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|z 9780080449579
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|z 0080449573
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|a CL0500000361
|b Safari Books Online
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|a TL571
|b .N37 2008
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|a 629.132305
|2 22
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| 049 |
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|a UAMI
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| 100 |
1 |
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|a Năstase, Adriana.
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| 245 |
1 |
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|a Computation of supersonic flow over flying configurations /
|c Adriana Nastase.
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| 250 |
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|a 1st ed.
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| 260 |
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|a London, UK ;
|a Burlington, MA :
|b Academic Press,
|c ©2008.
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| 300 |
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|a 1 online resource (1 volume) :
|b illustrations
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| 336 |
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|a text
|b txt
|2 rdacontent
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| 337 |
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|a computer
|b c
|2 rdamedia
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| 338 |
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|a online resource
|b cr
|2 rdacarrier
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| 588 |
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|a Print version record.
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| 504 |
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|a Includes bibliographical references and indexes.
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|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
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| 590 |
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|a O'Reilly
|b O'Reilly Online Learning: Academic/Public Library Edition
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| 650 |
|
0 |
|a Aerodynamics, Supersonic
|x Mathematical models.
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| 650 |
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0 |
|a Boundary value problems.
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| 650 |
|
0 |
|a Navier-Stokes equations.
|
| 650 |
|
6 |
|a Aérodynamique supersonique
|x Modèles mathématiques.
|
| 650 |
|
6 |
|a Problèmes aux limites.
|
| 650 |
|
6 |
|a Équations de Navier-Stokes.
|
| 650 |
|
7 |
|a Aerodynamics, Supersonic
|x Mathematical models
|2 fast
|
| 650 |
|
7 |
|a Boundary value problems
|2 fast
|
| 650 |
|
7 |
|a Navier-Stokes equations
|2 fast
|
| 776 |
0 |
8 |
|i Print version:
|a Năstase, Adriana.
|t Computation of supersonic flow over flying configurations.
|b 1st ed.
|d Amsterdam, The Netherlands ; Boston, Mass. : Elsevier, ©2008
|z 9780080449579
|w (DLC) 2010287989
|w (OCoLC)79447673
|
| 856 |
4 |
0 |
|u https://learning.oreilly.com/library/view/~/9780080449579/?ar
|z Texto completo (Requiere registro previo con correo institucional)
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| 938 |
|
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|a Coutts Information Services
|b COUT
|n 7446928
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| 938 |
|
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|a ProQuest MyiLibrary Digital eBook Collection
|b IDEB
|n 114469
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| 994 |
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|a 92
|b IZTAP
|
