Accession Number : AD0866498
Title : Propulsion System Flow Stability Program (Dynamic). Part III. RA-5C Accommodation Control System Simulation Program.
Descriptive Note : Final technical rept. 1 Oct 68-1 Dec 69 on Phase 2,
Corporate Author : NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV
Personal Author(s) : Lum, Evan L. ; Wong, Heeman W. ; Bayati, Jamal E.
Report Date : FEB 1970
Pagination or Media Count : 359
Abstract : This part of the report describes the dynamic simulation used to evaluate the RA-5C accommodation control in accommodating potentially dangerous disturbances which might jeopardize the normal operation and compromise the performance of the propulsion system. A dynamic analysis is necessary to verify the effectiveness of an accommodation control concept in taking corrective action in response to a disturbance. (Author)
Descriptors : (*RECONNAISSANCE AIRCRAFT, TURBOJET ENGINES), (*TURBOJET ENGINES, AXIAL FLOW COMPRESSORS), (*AXIAL FLOW COMPRESSORS, FLOW SEPARATION), STABILITY, DETECTORS, TRANSIENTS, SCREAMING COMBUSTION, TURBULENCE, THERMAL SHOCK, PREDICTIONS, MATHEMATICAL MODELS, FLOW CHARTING, COMPUTER PROGRAMS, ANALOG-DIGITAL COMPUTERS, TURBINE PARTS, ADVANCED WEAPONS.
Subject Categories : Patrol and Reconnaissance Aircraft
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE