Accession Number : AD0847095
Title : Inlet Distortion Investigation, Upstream Engine Influence and Screen Simulation.
Descriptive Note : Final rept.,
Corporate Author : BOEING CO SEATTLE WA
Personal Author(s) : Winslow, Larry J. ; Wendland, Daniel W. ; Smith, Brian D. ; Welliver, Albertus D.
Report Date : JAN 1969
Pagination or Media Count : 400
Abstract : This report describes the results of an investigation of the flow field at the discharge plane of an 0.28-scale SST-type inlet under ground test conditions, the up-stream influence of the compressor on the flow field at the discharge plane, and screen simulation of the flow field. The tests conducted with a YJ85-5 engine were: Test I - 0.28-scale inlet isolated from engine with constant-area duct; Test II - downstream decay of flow pattern from inlet discharge; Test III - 0.28-scale inlet close coupled to engine; Test IV - screen simulation of isolated inlet flow field; Test V - screen simulation of close-coupled inlet flow field. (Author)
Descriptors : (*TURBOJET ENGINES, AERODYNAMIC CHARACTERISTICS), (*TURBOJET INLETS, FLOW FIELDS), AIRCRAFT ENGINES, SUPERSONIC AIRCRAFT, TRANSPORT AIRCRAFT, CAPTIVE TESTS, SIMULATION, SCALE, DUCT INLETS, AXIAL FLOW COMPRESSORS, DISTORTION, MODEL TESTS, VORTICES, INSTRUMENTATION.
Subject Categories : Fluid Mechanics
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE