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Accession Number:
AD0856561
Title:
Propulsion System Flow Stability Program (Dynamic). Part I. Summary.
Descriptive Note:
Final technical rept. 20 Jun 67-30 Sep 68 on Phase 1,
Corporate Author:
NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV
Report Date:
1968-12-01
Pagination or Media Count:
174.0
Abstract:
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.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE