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|a dlr
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4 |
|a QC168
|b .E6 1986
|
| 082 |
0 |
4 |
|a 620.1/074
|2 19
|
| 049 |
|
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|a UAMI
|
| 100 |
1 |
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|a Emanuel, George.
|
| 245 |
1 |
0 |
|a Gasdynamics, theory and applications /
|c George Emanuel.
|
| 260 |
|
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|a New York, N.Y. :
|b American Institute of Aeronautics and Astronautics,
|c ©1986.
|
| 300 |
|
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|a 1 online resource (x, 451 pages) :
|b illustrations
|
| 336 |
|
|
|a text
|b txt
|2 rdacontent
|
| 337 |
|
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|a computer
|b c
|2 rdamedia
|
| 338 |
|
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|a online resource
|b cr
|2 rdacarrier
|
| 347 |
|
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|a data file
|
| 490 |
1 |
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|a AIAA education series
|
| 504 |
|
|
|a Includes bibliographical references and index.
|
| 506 |
|
|
|3 Use copy
|f Restrictions unspecified
|2 star
|5 MiAaHDL
|
| 533 |
|
|
|a Electronic reproduction.
|b [Place of publication not identified] :
|c HathiTrust Digital Library,
|d 2010.
|5 MiAaHDL
|
| 538 |
|
|
|a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.
|u http://purl.oclc.org/DLF/benchrepro0212
|5 MiAaHDL
|
| 583 |
1 |
|
|a digitized
|c 2010
|h HathiTrust Digital Library
|l committed to preserve
|2 pda
|5 MiAaHDL
|
| 588 |
0 |
|
|a Print version record.
|
| 505 |
0 |
|
|a Cover -- Title -- Copyright -- Foreword -- Table of Contents -- Introduction -- Thermodynamics -- One-Dimensional Conservation Equations -- Steady Streamtube Flow -- Noraml and Oblique Shock Waves -- Prandtl-Meyer Flow and Shock-Expansion Theory -- Nozzle and Diffuser Flow -- Ducts with Area Change, Heat Transfer, and Friction -- Unsteady, One-Dimensional Flow -- Applications of Unsteady, One-Dimensional Flow -- Governing Equations -- Shock Waves -- Transformation of the Conservation Equations -- Definitions and Theorems
|
| 505 |
8 |
|
|a Exact Solutions of Steady Homentropic Flow of a Perfect Gas Theory of Characteristics -- Minimum-Length Nozzles -- Aerodynamic Window -- Flows with Shock Waves -- Waverider Aerodynamics -- SI Units and Nomenclature -- Thermodynamic Summary -- Streamtube Flow Equations -- Normal and Oblique Shock Summary -- Shock Wave Angle (beta) vs Flow Deflection Angle (theta) -- Prandtl-Meyer Flow Summary -- Shock-Expansion Summary -- Nozzle Flow Summary -- Summary of Equations for Ducts with Area Change, Heat Transfer, and Friction
|
| 505 |
8 |
|
|a Rayleigh Flow Summary Fanno Flow Summary -- Unsteady, Normal Shock Summary -- Reflected Shock Wave Summary -- Jacobian Theory -- Subject Index
|
| 590 |
|
|
|a ProQuest Ebook Central
|b Ebook Central Academic Complete
|
| 650 |
|
0 |
|a Gas dynamics.
|
| 650 |
|
0 |
|a Fluid dynamics.
|
| 650 |
|
0 |
|a Aerodynamics, Supersonic.
|
| 650 |
|
2 |
|a Hydrodynamics
|
| 650 |
|
6 |
|a Dynamique des gaz.
|
| 650 |
|
6 |
|a Dynamique des fluides.
|
| 650 |
|
6 |
|a Aérodynamique supersonique.
|
| 650 |
|
7 |
|a Aerodynamics, Supersonic
|2 fast
|
| 650 |
|
7 |
|a Fluid dynamics
|2 fast
|
| 650 |
|
7 |
|a Gas dynamics
|2 fast
|
| 758 |
|
|
|i has work:
|a Gasdynamics (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCYDXgGyRTGtvDdVpVx3qQq
|4 https://id.oclc.org/worldcat/ontology/hasWork
|
| 776 |
0 |
8 |
|i Print version:
|a Emanuel, George.
|t Gasdynamics, theory and applications.
|d New York, N.Y. : American Institute of Aeronautics and Astronautics, ©1986
|z 0930403126
|z 9780930403126
|w (DLC) 86010771
|w (OCoLC)13644093
|
| 830 |
|
0 |
|a AIAA education series.
|
| 856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111548
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