Distributed Educated Throat Stability Bypass To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 60 Percent Internal Contraction
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Distributed Educated Throat Stability Bypass To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 60 Percent Internal Contraction
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Author : Robert Joseph Shaw
language : en
Publisher:
Release Date : 1974
Distributed Educated Throat Stability Bypass To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 60 Percent Internal Contraction written by Robert Joseph Shaw and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aerodynamics, Supersonic categories.
The results of an experimental investigation to increase the stable airflow operating range of a supersonic mixed-compression inlet are presented. A distributed educated throat stability-bypass entrance configuration was tested. In terms of diffuser-exit corrected airflow, a large inlet stable airflow range of about 16.1 percent was obtained if a constant pressure was maintained in the bypass plenum. Limited unstart angle of attack data are presented.
Throat Stability Bypass Systems To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 60 Percent Internal Contraction
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Author : Glenn A. Mitchell
language : en
Publisher:
Release Date : 1974
Throat Stability Bypass Systems To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 60 Percent Internal Contraction written by Glenn A. Mitchell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aerodynamics, Supersonic categories.
Nasa Technical Paper
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Author :
language : en
Publisher:
Release Date : 1980
Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Science categories.
Distributed Porous Throat Stability Bypass To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 60 Percent Internal Contraction
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Author : Robert Joseph Shaw
language : en
Publisher:
Release Date : 1974
Distributed Porous Throat Stability Bypass To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 60 Percent Internal Contraction written by Robert Joseph Shaw and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aerodynamics, Supersonic categories.
The results of an experimental investigation to increase the stable airflow operating range of a supersonic, mixed-compression inlet with 60-percent internal contraction are presented. Various distributed-porous, throat stability-bypass entrance configurations were tested. In terms of diffuser-exit corrected airflow, a large inlet stable airflow range of about 25 percent was obtained with the optimum configuration if a constant pressure was maintained in the by-pass plenum. The location of the centerbody bleed region had a decided effect on the overall inlet performance. Limited unstart angle-of-attack data are presented.
Nasa Technical Paper
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1980
Nasa Technical Paper written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Aeronautics categories.
Nasa Technical Memorandum
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Author :
language : en
Publisher:
Release Date : 1974
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 1974 with Aeronautics categories.
Forward Slanted Slot Throat Stability Bypass To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 60 Percent Internal Contraction
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Author : Robert Joseph Shaw
language : en
Publisher:
Release Date : 1974
Forward Slanted Slot Throat Stability Bypass To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 60 Percent Internal Contraction written by Robert Joseph Shaw and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aerodynamics, Supersonic categories.
Dynamic Response Of A Mach 2 5 Axisymmetric Inlet And Turbojet Engine With A Poppet Valve Controlled Inlet Stability Bypass System When Subjected To Internal And External Airflow Transients
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Author : Bobby W. Sanders
language : en
Publisher:
Release Date : 1980
Dynamic Response Of A Mach 2 5 Axisymmetric Inlet And Turbojet Engine With A Poppet Valve Controlled Inlet Stability Bypass System When Subjected To Internal And External Airflow Transients written by Bobby W. Sanders and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Airplanes categories.
Dynamic Response Of A Mach 2 5 Axisymmetric Inlet And Turbojet Engine With A Poppet Value Controlled Inlet Stability Bypass System When Subjected To Internal And External Airflow Transients
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1980
Dynamic Response Of A Mach 2 5 Axisymmetric Inlet And Turbojet Engine With A Poppet Value Controlled Inlet Stability Bypass System When Subjected To Internal And External Airflow Transients written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with categories.
Turbojet Exhaust Nozzle Secondary Airflow Pumping As An Exit Control Of An Inlet Stability Bypass System For A Mach 2 5 Axisymmetric Mixed Compression Inlet
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Author : Bobby W. Sanders
language : en
Publisher:
Release Date : 1980
Turbojet Exhaust Nozzle Secondary Airflow Pumping As An Exit Control Of An Inlet Stability Bypass System For A Mach 2 5 Axisymmetric Mixed Compression Inlet written by Bobby W. Sanders and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Airplanes categories.