Computational Method To Predict Thermodynamic Transport And Flow Properties For The Modified Langley 8 Foot High Temperature Tunnel
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Computational Method To Predict Thermodynamic Transport And Flow Properties For The Modified Langley 8 Foot High Temperature Tunnel
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Author : S. Venkateswaran
language : en
Publisher:
Release Date : 1992
Computational Method To Predict Thermodynamic Transport And Flow Properties For The Modified Langley 8 Foot High Temperature Tunnel written by S. Venkateswaran and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Aerothermodynamics categories.
Computational Method To Predict Thermodynamic Transport And Flow Properties For The Modified Langley 8 Foot High Temperature Tunnel
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Author : S. Venkateswaran
language : en
Publisher:
Release Date : 1992
Computational Method To Predict Thermodynamic Transport And Flow Properties For The Modified Langley 8 Foot High Temperature Tunnel written by S. Venkateswaran and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with categories.
Computational Method To Predict Thermodynamic Transport And Flow Properties For The Modified Langley 8 Foot High Temperature Tunnel
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-02
Computational Method To Predict Thermodynamic Transport And Flow Properties For The Modified Langley 8 Foot High Temperature Tunnel written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-02 with categories.
The Langley 8 foot high temperature tunnel (8 ft HTT) is used to test components of hypersonic vehicles for aerothermal loads definition and structural component verification. The test medium of the 8 ft HTT is obtained by burning a mixture of methane and air under high pressure; the combustion products are expanded through an axisymmetric conical contoured nozzle to simulate atmospheric flight at Mach 7. This facility was modified to raise the oxygen content of the test medium to match that of air and to include Mach 4 and Mach 5 capabilities. These modifications will facilitate the testing of hypersonic air breathing propulsion systems for a wide range of flight conditions. A computational method to predict the thermodynamic, transport, and flow properties of the equilibrium chemically reacting oxygen enriched methane-air combustion products was implemented in a computer code. This code calculates the fuel, air, and oxygen mass flow rates and test section flow properties for Mach 7, 5, and 4 nozzle configurations for given combustor and mixer conditions. Salient features of the 8 ft HTT are described, and some of the predicted tunnel operational characteristics are presented in the carpet plots to assist users in preparing test plans. Venkateswaran, S. and Hunt, L. Roane and Prabhu, Ramadas K. Langley Research Center RTOP 506-43-31-05...
Nasa Technical Memorandum
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Author :
language : en
Publisher:
Release Date : 1992
Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Aeronautics categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1992
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Aeronautics categories.
Structural Testing Technology At High Temperature
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Author :
language : en
Publisher:
Release Date : 1991
Structural Testing Technology At High Temperature written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991 with High temperatures categories.
Aeronautical Engineering
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Author :
language : en
Publisher:
Release Date : 1993
Aeronautical Engineering written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Aeronautics categories.
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Aeronautical Engineering A Cumulative Index To A Continuing Bibliography Supplement 287
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Author :
language : en
Publisher:
Release Date : 1993
Aeronautical Engineering A Cumulative Index To A Continuing Bibliography Supplement 287 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with categories.
The Aeronautical Journal
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Author :
language : en
Publisher:
Release Date : 1992
The Aeronautical Journal written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Aeronautics categories.
Monthly Catalogue United States Public Documents
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Author :
language : en
Publisher:
Release Date : 1993-03
Monthly Catalogue United States Public Documents written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993-03 with Government publications categories.