Accession Number:

AD0856561

Title:

Propulsion System Flow Stability Program (Dynamic). Part I. Summary.

Descriptive Note:

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

Corporate Author:

NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV

Personal Author(s):

• Martin, Arnold W.

Report Date:

1968-12-01

Pagination or Media Count:

174.0

Abstract:

Contents Identification of transients Inlet dynamic distortion Compressor response to spatial and time-variant distortion Compressor response to circumferential and radial distortion Unsteady combustion in duct burners Numerical definition of engine face distortion Stability margin performance penalties Survey of sensors applicable to the control of aircraft propulsion systems Simulation program development.

Descriptors:

• (*TURBOJET ENGINES
• PERFORMANCE(ENGINEERING))
• AERODYNAMIC CHARACTERISTICS
• TURBOFAN ENGINES
• STABILITY
• TURBULENCE
• TRANSIENTS
• TURBOJET INLETS
• AXIAL FLOW COMPRESSORS
• DISTORTION
• COMBUSTION
• AIRCRAFT ENGINES
• SIMULATION
• REVIEWS

Subject Categories:

• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE