Accession Number:

AD0856229

Title:

Propulsion System Integration and Test Program (Steady State)-Summary. Part I. Integration Technique and Test Activities.

Descriptive Note:

Final technical rept. Jun 67-Feb 69,

Corporate Author:

NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV

Personal Author(s):

• Johnson, Robert H.

Report Date:

1969-06-01

Pagination or Media Count:

239.0

Abstract:

The report describes a propulsion systemairplane integration technique and summarizes the results of six test programs conducted during the study. The six tests were Thrust divertervectoring system flow tests Shared exit ejector nozzle static tests Nozzle interaction drag tests Inlet drag tests Low speed auxiliary inlet tests and YTF-33 turbofan engine tests. Author

Descriptors:

• *TURBOFAN ENGINES
• PERFORMANCE(ENGINEERING)
• INTEGRATED SYSTEMS
• OPTIMIZATION
• AIRCRAFT MODELS
• TURBOJET EXHAUST NOZZLES
• TURBOJET INLETS
• AIRFRAMES
• WEIGHT
• WIND TUNNEL MODELS
• MISSION PROFILES
• INTERFACES
• INTERACTIONS
• TEST METHODS

Subject Categories:

• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE