Accession Number:

AD0503304

Title:

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

Personal Author(s):

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

Communities Of Interest:

Contract Number:

F33615-67-C-1848

File Size:

0.00MB

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