DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
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
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
Distribution Statement:
APPROVED FOR PUBLIC RELEASE