Propulsion System Flow Stability Program (Dynamic). Part I. Summary.

Abstract

Contents: Identification of transients; Inlet dynamic distortion; Compressor response to spatial and time-variant distortion; Compressor response to circumferential and radial distortion; Unsteady combustion in duct burners; Numerical definition of engine face distortion; Stability margin performance penalties; Survey of sensors applicable to the control of aircraft propulsion systems; Simulation program development.

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1968
Accession Number
AD0856561

Entities

People

  • Arnold W. Martin

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Combustion
  • Compressors
  • Distortion
  • Identification
  • Propulsion Systems
  • Simulations

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerodynamics.
  • Electrical Engineering