Work

Modification of axial compressor streamline program for analysis of engine test data

Year: 1979

Type: article

Abstract: An existing axial compressor streamline analysis computer program to allow input of measured radial pressure and temperature profiles obtained from engine or cascade data is described. The proposed modifications increase the input flexibility and are accomplished without changing the computer program's input format.

Source: NASA STI Repository (National Aeronautics and Space Administration)

Author: John G. Williams

Institution: Glenn Research Center

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: green

OpenAlex ID: W778436262

FWCI:

Cites: 2

Cited by:

Related to: 10