Analysis Of Dynamic Performance Limitations Of Fast Response 150 To 200 Hz Electrohydraulic Servos
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United States. National Aeronautics and Space Administration Scientific and Technical Information Division
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
NASA Scientific and Technical Reports by United States. National Aeronautics and Space Administration Scientific and Technical Information Division Pdf
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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
A Selected Listing of NASA Scientific and Technical Reports by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Pdf
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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
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 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.
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.
United States. National Aeronautics and Space Administration
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
Author : United States. Superintendent of Documents Publisher : Unknown Page : 1504 pages File Size : 50,9 Mb Release : 1979 Category : United States ISBN : STANFORD:36105019598296