Coverart for item
The Resource Hypersonic Flow Research

Hypersonic Flow Research

Label
Hypersonic Flow Research
Title
Hypersonic Flow Research
Creator
Contributor
Subject
Genre
Language
eng
Cataloging source
MiAaPQ
LC call number
TL571.5 -- .I58 1961eb
Literary form
non fiction
Nature of contents
dictionaries
Label
Hypersonic Flow Research
Link
http://ebookcentral.proquest.com/lib/multco/detail.action?docID=3111465
Instantiates
Publication
Copyright
Carrier category
online resource
Carrier category code
cr
Carrier MARC source
rdacarrier
Color
multicolored
Content category
text
Content type code
txt
Content type MARC source
rdacontent
Contents
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 -- 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 -- 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 -- Air Arc Simulation of Hypersonic Environments -- Development of the Shock Tunnel and Its Application to Hypersonic Flight
Control code
EBC3111465
Dimensions
unknown
Extent
1 online resource (768 pages)
Form of item
online
Isbn
9781600862625
Media category
computer
Media MARC source
rdamedia
Media type code
c
Note
Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2017. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
Sound
unknown sound
Specific material designation
remote
System control number
  • (MiAaPQ)EBC3111465
  • (Au-PeEL)EBL3111465
  • (CaPaEBR)ebr10516465
  • (OCoLC)922978766
Label
Hypersonic Flow Research
Link
http://ebookcentral.proquest.com/lib/multco/detail.action?docID=3111465
Publication
Copyright
Carrier category
online resource
Carrier category code
cr
Carrier MARC source
rdacarrier
Color
multicolored
Content category
text
Content type code
txt
Content type MARC source
rdacontent
Contents
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 -- 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 -- 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 -- Air Arc Simulation of Hypersonic Environments -- Development of the Shock Tunnel and Its Application to Hypersonic Flight
Control code
EBC3111465
Dimensions
unknown
Extent
1 online resource (768 pages)
Form of item
online
Isbn
9781600862625
Media category
computer
Media MARC source
rdamedia
Media type code
c
Note
Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2017. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
Sound
unknown sound
Specific material designation
remote
System control number
  • (MiAaPQ)EBC3111465
  • (Au-PeEL)EBL3111465
  • (CaPaEBR)ebr10516465
  • (OCoLC)922978766

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