Author : Daniel I. Drain
Publisher :
Page : 44 pages
File Size : 50,96 MB
Release : 1969
Category : Jet propulsion
ISBN :
Dynamic tests for air breathing engines using sweep frequency techniques.
Author : Daniel I. Drain
Publisher :
Page : 32 pages
File Size : 25,81 MB
Release : 1969
Category :
ISBN :
Author : John R. Szuch
Publisher :
Page : 52 pages
File Size : 23,92 MB
Release : 1970
Category : Airplanes
ISBN :
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.
Author :
Publisher :
Page : 912 pages
File Size : 38,12 MB
Release : 1991
Category : Aeronautics
ISBN :
Author : United States. Superintendent of Documents
Publisher :
Page : 1464 pages
File Size : 36,85 MB
Release : 1966
Category : Government publications
ISBN :
Author : United States. Superintendent of Documents
Publisher :
Page : 1504 pages
File Size : 42,55 MB
Release : 1979
Category : United States
ISBN :
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher :
Page : 966 pages
File Size : 17,99 MB
Release : 1970
Category : Aeronautics
ISBN :
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher :
Page : 962 pages
File Size : 10,65 MB
Release : 1970
Category : Aeronautics
ISBN :
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher :
Page : 956 pages
File Size : 18,54 MB
Release : 1970
Category : Science
ISBN :
Author : Francis J. Paulovich
Publisher :
Page : 52 pages
File Size : 37,86 MB
Release : 1971
Category : Airplanes
ISBN :
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.
