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Accession Number:
AD0847095
Title:
Inlet Distortion Investigation, Upstream Engine Influence and Screen Simulation.
Corporate Author:
BOEING CO SEATTLE WA
Report Date:
1969-01-01
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
Descriptive Note:
Final rept.,
Pages:
0400
Contract Number:
F33615-68-C-1094
File Size:
0.00MB
