NASA Technical Reports Server (NTRS) : Low pdf

NASA Technical Reports Server (NTRS) : Low

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This paper presents a dynamic model of an internal combustion engine coupled to a variable pitch propeller. The low-order, nonlinear time-dependent model is useful for simulating the propulsion system of general aviation single-engine light aircraft. This model is suitable for investigating engine diagnostics and monitoring and for control design and development. Furthermore, the model may be extended to provide a tool for the study of engine emissions, fuel economy, component effects, alternative fuels, alternative engine cycles, flight simulators, sensors, and actuators. Results show that the model provides a reasonable representation of the propulsion system dynamics from zero to 10 Hertz

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 7/1/1995
• Year: 1995
• Book Topics/Themes: NASA Technical Reports Server (NTRS), AIRCRAFT MODELS, DYNAMIC MODELS, FLIGHT SIMULATION, GENERAL AVIATION AIRCRAFT, INTERNAL COMBUSTION ENGINES, PROPULSION SYSTEM PERFORMANCE, SINGLE ENGINE AIRCRAFT, VARIABLE PITCH PROPELLERS, FUEL FLOW, FUEL-AIR RATIO, INTAKE SYSTEMS, LIGHT AIRCRAFT, MATHEMATICAL MODELS, Richard, Jacques C

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