Stability Margin Definition

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.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1970
Accession Number
AD0874880

Entities

People

  • Brian Brimelow

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Back Pressure
  • Compressors
  • Computer Simulations
  • Engine Components
  • Engines
  • Flow Fields
  • Government (Foreign)
  • Governments
  • Instrumentation
  • Mathematical Models
  • Propulsion Systems
  • Q Factor
  • Simulations
  • Steady State
  • Turbofan Engines

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Theoretical Analysis.