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

Personal Author(s) : Martin, Arnold W.

Report Date : DEC 1968

Pagination or Media Count : 174

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.

Descriptors :   (*TURBOJET ENGINES, PERFORMANCE(ENGINEERING)), AERODYNAMIC CHARACTERISTICS, TURBOFAN ENGINES, STABILITY, TURBULENCE, TRANSIENTS, TURBOJET INLETS, AXIAL FLOW COMPRESSORS, DISTORTION, COMBUSTION, AIRCRAFT ENGINES, SIMULATION, REVIEWS.

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE