Servosystem Design of a High-response Slotted-plate Overboard Bypass Valve for a Supersonic Inlet PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Servosystem Design of a High-response Slotted-plate Overboard Bypass Valve for a Supersonic Inlet PDF full book. Access full book title Servosystem Design of a High-response Slotted-plate Overboard Bypass Valve for a Supersonic Inlet by George H. Neiner. Download full books in PDF and EPUB format.
Author: George H. Neiner
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 28
Get Book Here
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: George H. Neiner
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 28
Get Book Here
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: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1290
Get Book Here
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 624
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388
Get Book Here
Book Description
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1408
Get Book Here
Book Description
Author: John A. Webb
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 56
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 62
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 512
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 792
Get Book Here
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.
