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

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE