Equilibrium operating performance of axial-flow turbojet engines by means of idealized analysis /
John C. Sanders and Edward C. Chapin.

Description

Main Author

Sanders, John C.

Related Names

Chapin, Edward C.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1949.

Subjects

Mathematical analysis.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Performance.

Summary

This investigation was made for an engine in which the ratio of axial-inlet-air velocity to compressor-tip velocity is constant, which approximates operation of turbojet engines with axial-flow compressors.
A method for predicting equilibrium operating performance of turbojet engines has been developed, with the assumption of simple model processes for the components. Results of the analysis are plotted graphically in terms of dimensionless parameters consisting of critical engine dimensions and over-all operating variables.

Note

NACA TN No. 1956.
"October 1949."

Physical Description

40 p. : ill. ; 28 cm.

Locate a Print Version

Find in a library

Viewability