Accession Number : ADA182635

Title :   Engine Response to Distorted Inflow Conditions: Conference Proceedings of the Propulsion and Energetics Specialists' Meeting (68th) Held in Munich, Germany on 8-9 September 1986.

Corporate Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

PDF Url : ADA182635

Report Date : Mar 1987

Pagination or Media Count : 305

Abstract : This meeting opened with a review of current knowledge on the meeting subject arranged in the following sessions: Unsteady Flow and Validation of Empirical Distortion Parameters (3); Computation Technique for Engine/Compressor Performance Predictions of Distorted Inflow (5); Characterization of Distorted Inflow (4); and Experimental Investigations of Engine Instability and Response to Flow Distortion (3). These proceedings contain 16 papers. The meeting was intended to provide scientists and development engineers with a broad information on acceptable inflow distortion parameters to be applied to airframe-intake integration, computation technique for engine/compressor performance prediction of distorted inflow, distortion inflow detection, and experimental investigation of engine instability.

Descriptors :   *AIR INTAKES, *UNSTEADY FLOW, *JET ENGINES, *SYMPOSIA, *COMPRESSORS, PRESSURE DISTRIBUTION, TEMPERATURE, DISTORTION, STABILITY, NONUNIFORM FLOW, DYNAMIC RESPONSE, PERFORMANCE(ENGINEERING), COMPUTER AIDED DESIGN, JET ENGINE INLETS, AIRFRAMES, COMPATIBILITY, EDDIES(FLUID MECHANICS)

Subject Categories : Fluid Mechanics
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE