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Accession Number:
AD0503304
Title:
Propulsion System Flow Stability Program (Dynamic). Part XIV. Propulsion System Stability Margin Performance Penalties for an RA-5C Aircraft.
Corporate Author:
NORTH AMERICAN ROCKWELL CORP LOS ANGELES CALIF LOS ANGELES DIV
Report Date:
1968-12-01
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
Descriptive Note:
Final technical rept. 20 Jun 67-30 Sep 68 on Phase 1,
Supplementary Note:
See also Part 15, AD-503 328.
Pages:
0073
Contract Number:
F33615-67-C-1848
File Size:
0.00MB
