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Propulsion System Flow Stability Program (Dynamic). Part I. Summary.
Final technical rept. 20 Jun 67-30 Sep 68 on Phase 1,
NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV
Pagination or Media Count:
Contents Identification of transients Inlet dynamic distortion Compressor response to spatial and time-variant distortion Compressor response to circumferential and radial distortion Unsteady combustion in duct burners Numerical definition of engine face distortion Stability margin performance penalties Survey of sensors applicable to the control of aircraft propulsion systems Simulation program development.
APPROVED FOR PUBLIC RELEASE