Accession Number:

AD0503304

Title:

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

Descriptive Note:

Final technical rept. 20 Jun 67-30 Sep 68 on Phase 1,

Corporate Author:

NORTH AMERICAN ROCKWELL CORP LOS ANGELES CALIF LOS ANGELES DIV

Personal Author(s):

Report Date:

1968-12-01

Pagination or Media Count:

73.0

Abstract:

Steady state propulsion system and aircraft performance penalties due to control margins required for transient operation were studied for the RA-5C aircraftJ79 engine configuration. Significant performance gains were made when these margins could be reduced and a smaller turbine used. Author

Subject Categories:

  • Bombers
  • Attack and Fighter Aircraft
  • Patrol and Reconnaissance Aircraft
  • Fluid Mechanics
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE