Restart and High Response Terminal Shock Control for an Axisymmetric Mixed-compression Inlet with 60-percent Internal Contraction PDF Download
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Author: Michael J. Crosby
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
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Author: Michael J. Crosby
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
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Book Description
Author: Michael J. Crosby
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Author: Gary L. Cole
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 956
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
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Book Description
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.
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
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Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
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Author: George H. Neiner
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 28
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Book Description
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.
Author: Francis J. Paulovich
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
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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.
Author: Glenn A. Mitchell
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 108
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