Propulsion System Flow Stability Program (Dynamic). Part XIV. Propulsion System Stability Margin Performance Penalties for an RA-5C Aircraft.

Abstract

Steady state propulsion system and aircraft performance penalties due to control margins required for transient operation were studied for the RA-5C aircraft/J79 engine configuration. Significant performance gains were made when these margins could be reduced and a smaller turbine used. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1968
Accession Number
AD0503304

Entities

People

  • Ray M. Tyson

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Propulsion Systems
  • Steady State

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Control Systems Engineering.