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151017s2000 xx o 000 0 eng d |
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|a EBLCP
|b eng
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|c EBLCP
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|d OCLCQ
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|a 9781600862625
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|a 1600862624
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|a DEBBG
|b BV044094773
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|a (OCoLC)922978766
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|a TL571.5 ǂb I58 1961eb
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|a 629.13232
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|a UAMI
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|a Riddell, Frederick R.
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|a Hypersonic Flow Research.
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|a Reston :
|b American Institute of Aeronautics and Astronautics,
|c 2000.
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|a 1 online resource (768 pages)
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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 online resource
|b cr
|2 rdacarrier
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|a Print version record.
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|a ""Cover""; ""Title""; ""Copyright""; ""Hypersonics Committee""; ""Preface""; ""Contents""; ""The ARS � AFOSR International Hypersonics Conference: Summary and Comments""; ""A. Hypersonic Flow at Low Reynolds Number""; ""Introduction""; ""Density Behavior along the Stagnation Line of a Blunt Body in Hyperthermal Flow""; ""Second-Order Compressible Boundary Layer Theory with Application to Blunt Bodies in Hypersonic Flow""; ""Comment on above paper""; ""Rarefied Hypersonic Flow over a Sphere""; ""The Rayleigh Problem for a Dissociated Gas""; ""B. Chemical Kinetic Effects in Hypersonic Flow""
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|a ""Introduction""""Chemical Kinetics: A General Introduction""; ""Chemical Kinetics of High Temperature Air""; ""Chemical Effects in External Hypersonic Flows""; ""Radiation at Hypersonic Speeds""; ""Radiation from the Nonequilibrium Shock Front""; ""C. Inviscid Hypersonic Flow""; ""Introduction""; ""Slender Wings at High Angles of Attack in Hypersonic Flows""; ""Newtonian Theory of Hypersonic Flow at Large Distances from Bluff Axially Symmetric Bodies""; ""Shock Layer Structure and Entropy Layers in Hypersonic Conical Flows""; ""Theory of Entropy Layers and Nose Bluntness in Hypersonic Flow""
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|a ""D. Experimental Techniques I""""Introduction""; ""Aerodynamic Testing at Mach Numbers from 15 to 20""; ""The Duration and Properties of the Flow in a Hypersonic Shock Tunnel""; ""An Evaluation of the Hypersonic Gun Tunnel""; ""Diagnostic Studies of a Low Density, Arc Heated Wind Tunnel Stream""; ""Initial Results from a Low Density, Hypervelocity Wind Tunnel""; ""E. Experimental Techniques II""; ""Introduction""; ""The Free Flight Range: A Tool for Research in the Physics of High Speed Flight""; ""Survey of Shock Tube Research Related to the Aerophysics Problem of Hypersonic Flight""
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|a ""Air Arc Simulation of Hypersonic Environments""""Development of the Shock Tunnel and Its Application to Hypersonic Flight""
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
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650 |
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|a Aerodynamics, Hypersonic
|v Congresses.
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650 |
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|a Aérodynamique hypersonique
|v Congrès.
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650 |
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|a Aerodynamics, Hypersonic
|2 fast
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655 |
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|a Conference papers and proceedings
|2 fast
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758 |
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|i has work:
|a Hypersonic Flow Research (Text)
|1 https://id.oclc.org/worldcat/entity/E39PD3vYqgfPbmfPjRjVkcG3ry
|4 https://id.oclc.org/worldcat/ontology/hasWork
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776 |
0 |
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|i Print version:
|a Riddell, Frederick R.
|t Hypersonic Flow Research.
|d Reston : American Institute of Aeronautics and Astronautics, ©2000
|z 9781563478567
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856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111465
|z Texto completo
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938 |
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|a ProQuest Ebook Central
|b EBLB
|n EBL3111465
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994 |
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|a 92
|b IZTAP
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