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140116s2008 enka ob 001 0 eng d |
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20240829144835.9 |
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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
|q (Cloth)
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|b 882723065
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|a (OCoLC)safo868231823
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|a (OCoLC)868231823
|z (OCoLC)313649720
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|a safo9780080449579
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|a UMI
|b eng
|e pn
|c UMI
|d CDX
|d IDEBK
|d DEBBG
|d DEBSZ
|d OCLCQ
|d OCLCF
|d OCLCQ
|d CEF
|d NLE
|d UAB
|d AU@
|d OCLCQ
|d OCLCO
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|d OCLCQ
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|a GWRE
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|a TL571
|b .N37 2008
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|a Năstase, Adriana.
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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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|a 1 online resource (1 volume) :
|b illustrations
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a volume
|b nc
|2 rdacarrier
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|a Print version record.
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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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|a Aerodynamics, Supersonic
|x Mathematical models.
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|a Boundary value problems.
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|a Navier-Stokes equations.
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|a Aerodynamics, Supersonic
|x Mathematical models
|2 fast
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|a Boundary value problems
|2 fast
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|a Navier-Stokes equations
|2 fast
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|i has work:
|a Computation of supersonic flow over flying configurations (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCGdbCrbv97ywmBwTTCYQdP
|4 https://id.oclc.org/worldcat/ontology/hasWork
|
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://go.oreilly.com/UniOfColoradoBoulder/library/view/~/9780080449579/?ar
|z Full Text (via O'Reilly/Safari)
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915 |
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|a -
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956 |
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|a O'Reilly-Safari eBooks
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956 |
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|b O'Reilly Online Learning: Academic/Public Library Edition
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994 |
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|a 92
|b COD
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998 |
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|b Subsequent record output
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f |
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|i 6b9194fc-2197-5b6c-a427-4f0701be146c
|s 4c48c620-0e7d-55aa-a8ad-c014848ce5ea
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952 |
f |
f |
|p Can circulate
|a University of Colorado Boulder
|b Online
|c Online
|d Online
|e TL571 .N37 2008
|h Library of Congress classification
|i web
|n 1
|