Accession Number:

ADA002314

Title:

Rotating Engine Design and Cycle Analysis Program,

Descriptive Note:

Corporate Author:

AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1974-10-01

Pagination or Media Count:

65.0

Abstract:

This report describes a computer program titled Rotating Engine Design and Cycle Analysis Program. The program is capable of analyzing turbojets, two spool turbofans both front and aft fans, turboprops, turboprops, turboshafts, and subsonic burning ramjets. This program was developed with emphasis on high speed computation for cycle analysis and for propulsionflight control sensor analysis. It is capable of computation time in the order of a few milliseconds per cycle case. The report includes a description of the programs capabilities and limitations, special features, complete listing, sample input data, and corresponding sample output data.

Subject Categories:

  • Computer Programming and Software
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE