Accession Number:

AD0874880

Title:

Stability Margin Definition

Descriptive Note:

Technical rept. Jan 1968-Jun 1970

Corporate Author:

AIR FORCE AERO PROPULSION LAB WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1970-06-01

Pagination or Media Count:

29.0

Abstract:

The available stability margin of a turbine propulsion system is a function of a wide range of parameters, many of which are time dependent. Both internal and external effects are considered and the interactions between inlet and engine stability coefficients are discussed.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE