An Evaluation Of Nozzle Afterbody Code Ar02p
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Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1987
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 1987 with Aeronautics categories.
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Civil Engineering Hydraulics Abstracts
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Author :
language : en
Publisher:
Release Date : 1988
Civil Engineering Hydraulics Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with Hydraulic engineering categories.
An Evaluation Of Nozzle Afterbody Code Ar02p
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Author : Frederick C. Guyton
language : en
Publisher:
Release Date : 1986
An Evaluation Of Nozzle Afterbody Code Ar02p written by Frederick C. Guyton and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986 with categories.
A project was undertaken to develop a computational fluid dynamics (CFD) code for use in nozzle afterbody analysis. Objectives were to create a three-dimensional code capable of calculating afterbody flows with accuracy quantitatively close to the Navier-Stokes solutions, but which would use significantly fewer computer resources. The resulting program coupled an inverse boundary-layer routine with an Euler code and incorporated a jet plume. Calculations were made for the axisymmetric AGARD 15-deg boattail afterbody with variations in nozzle pressure ratio for Mach numbers 0.6 and 0.9, and compared with experimental results. The code predicted drag changes with NPR which showed the proper variations, but the code did not provide the accuracy required for typical nozzle afterbody analysis. (NPR = Nozzle total pressure to free stream static pressure ratio.).
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1986-10
Government Reports Announcements Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986-10 with Science categories.
Government Reports Annual Index
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Author :
language : en
Publisher:
Release Date : 199?
Government Reports Annual Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 199? with categories.
Government Reports Annual Index Keyword A L
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Author :
language : en
Publisher:
Release Date : 1986
Government Reports Annual Index Keyword A L written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986 with Government reports announcements & index categories.
An Evaluation Of Nozzle Afterbody Code
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Author : Frederick C. Guyton
language : en
Publisher:
Release Date : 1986
An Evaluation Of Nozzle Afterbody Code written by Frederick C. Guyton and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986 with Boundary layer categories.
An Evaluation Of Nozzle Afterbody Code
DOWNLOAD
Author : Frederick C. Guyton
language : en
Publisher:
Release Date : 1986
An Evaluation Of Nozzle Afterbody Code written by Frederick C. Guyton and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986 with Boundary layer categories.
Evaluation Of Reynolds Number And Tunnel Wall Porosity Effects On Nozzle Afterbody Drag At Transonic Mach Numbers
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Author : C. E. Robinson
language : en
Publisher:
Release Date : 1976
Evaluation Of Reynolds Number And Tunnel Wall Porosity Effects On Nozzle Afterbody Drag At Transonic Mach Numbers written by C. E. Robinson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Aerodynamics, Transonic categories.
An experimental investigation was conducted to study the effects of Reynolds number variation on isolated nozzle afterbody performance. A strut-mounted cone-cylinder model with three separate afterbody configurations for Aerospace Research and Development (AGARD) was used for this investigation. This program was conducted in two phases distinguished by the model size and the wind tunnels used to obtain the experimental results. The effect of tunnel wall porosity on nozzle afterbody (NAB) performance was investigated.
Evaluation Of Reynolds Number And Tunnel Wall Porosity Effects On Nozzle Afterbody Drag At Transonic Mach Numbers
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Author :
language : en
Publisher:
Release Date : 1976
Evaluation Of Reynolds Number And Tunnel Wall Porosity Effects On Nozzle Afterbody Drag At Transonic Mach Numbers written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with categories.
An experimental investigation was conducted to study the effects of Reynolds number variation on isolated nozzle afterbody performance. A strut-mounted cone-cylinder model with three separate afterbody configurations for Aerospace Research and Development (AGARD) was used for this investigation. This program was conducted in two phases distinguished by the model size and the wind tunnels used to obtain the experimental results. The effect of tunnel wall porosity on nozzle afterbody (NAB) performance was investigated.