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
      Fluid Mechanics
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE