Accession Number : AD0866497

Title :   Propulsion System Flow Stability Program (Dynamic). Part I. Summary.

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) : Martin, Arnold W.

Report Date : FEB 1970

Pagination or Media Count : 89

Abstract : This volume, Part I of ten parts, summarizes the Phase II portion of the 'Propulsion System Flow Stability Program (Dynamic).' In addition, it serves as a directory to Parts II through X wherein more detailed information is presented. (Author)

Descriptors :   (*RECONNAISSANCE AIRCRAFT, TURBOJET ENGINES), (*TURBOJET ENGINES, AXIAL FLOW COMPRESSORS), (*AXIAL FLOW COMPRESSORS, FLOW SEPARATION), STABILITY, DETECTORS, TRANSIENTS, SCREAMING COMBUSTION, JET MIXING FLOW, INTERACTIONS, WIND TUNNEL MODELS, POWER SPECTRA, MATHEMATICAL MODELS, COMPUTER PROGRAMMING, PREDICTIONS, ADVANCED WEAPONS.

Subject Categories : Aerodynamics
      Patrol and Reconnaissance Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE