[PDF] Restart And High Response Terminal Shock Control For An Axisymmetric Mixed Compression Inlet With 60 Percent Internal Contraction - eBooks Review

Restart And High Response Terminal Shock Control For An Axisymmetric Mixed Compression Inlet With 60 Percent Internal Contraction


Restart And High Response Terminal Shock Control For An Axisymmetric Mixed Compression Inlet With 60 Percent Internal Contraction
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Restart And High Response Terminal Shock Control For An Axisymmetric Mixed Compression Inlet With 60 Percent Internal Contraction


Restart And High Response Terminal Shock Control For An Axisymmetric Mixed Compression Inlet With 60 Percent Internal Contraction
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Author : Michael J. Crosby
language : en
Publisher:
Release Date : 1969

Restart And High Response Terminal Shock Control For An Axisymmetric Mixed Compression Inlet With 60 Percent Internal Contraction written by Michael J. Crosby and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with categories.




An Automatic Restart Control System For An Axisymmetric Mixed Compression Inlet


An Automatic Restart Control System For An Axisymmetric Mixed Compression Inlet
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Author : Gary L. Cole
language : en
Publisher:
Release Date : 1969

An Automatic Restart Control System For An Axisymmetric Mixed Compression Inlet written by Gary L. Cole and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Airplanes categories.




Nasa Scientific And Technical Reports


Nasa Scientific And Technical Reports
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Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
language : en
Publisher:
Release Date : 1970

Nasa Scientific And Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Aeronautics categories.




Nasa Scientific And Technical Reports And Publications For 1969 A Selected Listing


Nasa Scientific And Technical Reports And Publications For 1969 A Selected Listing
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Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
language : en
Publisher:
Release Date : 1970

Nasa Scientific And Technical Reports And Publications For 1969 A Selected Listing written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Science categories.




Scientific And Technical Aerospace Reports


Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date :

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 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.



A Selected Listing Of Nasa Scientific And Technical Reports


A Selected Listing Of Nasa Scientific And Technical Reports
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Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
language : en
Publisher:
Release Date : 1970

A Selected Listing Of Nasa Scientific And Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Aeronautics categories.




Servosystem Design Of A High Response Slotted Plate Overboard Bypass Valve For A Supersonic Inlet


Servosystem Design Of A High Response Slotted Plate Overboard Bypass Valve For A Supersonic Inlet
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Author : George H. Neiner
language : en
Publisher:
Release Date : 1970

Servosystem Design Of A High Response Slotted Plate Overboard Bypass Valve For A Supersonic Inlet written by George H. Neiner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Jet engines categories.


The servosystem design of a high-response airflow bypass valving system for supersonic mixed-compression inlets or other industrial or aerospace pneumatic systems is described. The valve utilizes a multislotted plate to achieve flow area change with minimum stroke and mass of moving parts. The servosystem utilizes a hydraulic piston-in-cylinder actuator close-coupled to a two-stage electrohydraulic servovalve. Using electronic compensation the small-amplitude response of the system, modulating 14 percent of its full flow area, is flat within 0 to -3 dB to 110 Hz. (161 cm [to the second power] ). A mathematical model of the system is presented and analytical responses are compared with experimental data.



A Supersonic Inlet Engine Control Using Engine Speed As A Primary Variable For Controlling Normal Shock Position


A Supersonic Inlet Engine Control Using Engine Speed As A Primary Variable For Controlling Normal Shock Position
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Author : Francis J. Paulovich
language : en
Publisher:
Release Date : 1971

A Supersonic Inlet Engine Control Using Engine Speed As A Primary Variable For Controlling Normal Shock Position written by Francis J. Paulovich and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Airplanes categories.


A cross-coupled inlet-engine control system concept is presented for a supersonic propulsion system consisting of a mixed- compression inlet and a turbojet engine. The control system employs manipulation of both bypass door flow area and engine speed to stabilize normal shock position in the inlet. Specifically, the case of slow-acting bypass doors used as a reset control where engine speed is the primary means of shock position control is described. Experimental results are presented showing performance of the control system with a NASA-designed inlet and a turbojet engine operating at Mach 2.5 in the Lewis 10- by 10-Foot Supersonic Wind Tunnel.



Nasa Technical Note


Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1970

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with categories.




Pressure Activated Stability Bypass Control Valves To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 40 Percent Internal Contraction


Pressure Activated Stability Bypass Control Valves To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 40 Percent Internal Contraction
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Author : Glenn A. Mitchell
language : en
Publisher:
Release Date : 1974

Pressure Activated Stability Bypass Control Valves To Increase The Stable Airflow Range Of A Mach 2 5 Inlet With 40 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.