Analysis Of Dynamic Performance Limitations Of Fast Response 150 To 200 Hz Electrohydraulic Servos

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NASA Technical Note

Author : Anonim
Publisher : Unknown
Page : 730 pages
File Size : 54,7 Mb
Release : 1976
Category : Electronic
ISBN : MINN:31951000846579G

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NASA Technical Note by Anonim Pdf

NASA Tech Brief

Author : United States. National Aeronautics and Space Administration Technology Utilization Division
Publisher : Unknown
Page : 698 pages
File Size : 45,8 Mb
Release : 2024-06-29
Category : Electronic
ISBN : STANFORD:36105113794304

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NASA Tech Brief by United States. National Aeronautics and Space Administration Technology Utilization Division Pdf

NASA Scientific and Technical Reports

Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher : Unknown
Page : 966 pages
File Size : 47,6 Mb
Release : 1970
Category : Aeronautics
ISBN : STANFORD:36105113793769

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NASA Scientific and Technical Reports by United States. National Aeronautics and Space Administration Scientific and Technical Information Division Pdf

A Selected Listing of NASA Scientific and Technical Reports

Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher : Unknown
Page : 962 pages
File Size : 45,8 Mb
Release : 1970
Category : Aeronautics
ISBN : CORNELL:31924057848867

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A Selected Listing of NASA Scientific and Technical Reports by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Pdf

NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing

Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher : Unknown
Page : 956 pages
File Size : 50,7 Mb
Release : 1970
Category : Science
ISBN : NASA:31769000659238

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NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Pdf

Study of Turbojet Combustor Dynamics Using Sweep-frequency Data

Author : John R. Szuch,Francis J. Paulovich,William M. Bruton
Publisher : Unknown
Page : 52 pages
File Size : 51,6 Mb
Release : 1970
Category : Airplanes
ISBN : UIUC:30112106880468

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Study of Turbojet Combustor Dynamics Using Sweep-frequency Data by John R. Szuch,Francis J. Paulovich,William M. Bruton Pdf

The analysis of data obtained from sweep-frequency testing of the 585 turbojet combustor is discussed.Bode plots of the response of combustor pressure to sinusoidal disturbances in fuelspray- nozzle pressure are presented for a range of fuel flows. An analog simulation was developed and used to match the experimental data and to identify the combustion dynamics. The effects of primary or burning-zone fuel-to-air ratio on the system response were also investigated. The experimental data were fit by linear transfer function forms to be used in overall system studies.

NASA Technical Paper

Author : Anonim
Publisher : Unknown
Page : 40 pages
File Size : 40,9 Mb
Release : 1980
Category : Science
ISBN : STANFORD:36105024697547

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NASA Technical Paper by Anonim Pdf

Servosystem Design of a High-response Slotted-plate Overboard Bypass Valve for a Supersonic Inlet

Author : George H. Neiner
Publisher : Unknown
Page : 28 pages
File Size : 42,6 Mb
Release : 1970
Category : Jet engines
ISBN : UIUC:30112106880435

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Servosystem Design of a High-response Slotted-plate Overboard Bypass Valve for a Supersonic Inlet by George H. Neiner Pdf

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.

NASA Technical Paper

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 44 pages
File Size : 49,8 Mb
Release : 1980
Category : Aeronautics
ISBN : UOM:39015022339199

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NASA Technical Paper by United States. National Aeronautics and Space Administration Pdf

Monthly Catalog of United States Government Publications, Cumulative Index

Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1504 pages
File Size : 50,9 Mb
Release : 1979
Category : United States
ISBN : STANFORD:36105019598296

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Monthly Catalog of United States Government Publications, Cumulative Index by United States. Superintendent of Documents Pdf