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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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.
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.
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.
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 : 1975
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 1975 with Aeronautics categories.
Poppet Valve Control Of Throat Stability Bypass To Increase 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 : 1975
Poppet Valve Control Of Throat Stability Bypass To Increase 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 1975 with Aerodynamics, Supersonic categories.
The throat of a Mach 2.5 inlet with a coldpipe termination was fitted with a stability-bypass system. System variations included several stability bypass entrance configurations. Poppet valves controlled the bypass airflow. The inlet stable airflow range achieved with each configuration was determined for both steady state conditions and internal pulse transients. Results are compared with those obtained without a stability bypass system. Transient results were also obtained for the inlet with a choke point at the diffuser exit and for the inlet with large and small stability bypass plenum volumes. Poppet valves at the stability bypass exit provided the inlet with a stable airflow range of 20 percent or greater at all static and transient conditions.
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 Value Controlled Inlet Stability Bypass System When Subjected To Internal And External Airflow Transients
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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.
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.
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.