Accession Number:
AD0875187
Title:
A Problem in Matching an Inlet and Engine Having Steady-State Circumferential Inlet Pressure Distortion,
Descriptive Note:
Corporate Author:
NAVAL AIR PROPULSION TEST CENTER TRENTON NJ AERONAUTICAL TURBINE DEPT
Personal Author(s):
Report Date:
1970-08-01
Pagination or Media Count:
16.0
Abstract:
An analysis was made of the flow redistribution which occurs at the exit of an inlet due to the presence of a compressor. The flow redistribution includes a change in the axial velocity distortion, which is a function of the slope of the curve of compressor pressure coefficient versus flow coefficient at a particular corrected speed. Author
Descriptors:
Subject Categories:
- Jet and Gas Turbine Engines