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Advances in aerospace propulsion : SP-594 / Society of Automotive Engineers.

Por: Tipo de material: TextoTextoDetalles de publicación: Warrendale : Society of Automotive Engineers, 1984.Descripción: 160 p. : ilISBN:
  • 0898838150
Tema(s): Alcance y contenido: Design and experimental evaluation of propfan inlets - Engine inlet interaction with a prop-fan propulsion system - Stability and control results for advanced turboprop aft-mount installations - Aerodynamic test results for a wing-mounted turboprop propulsion installation - Advanced research instrumentation for aircraft turbomachinery - Acquisition of detailed heat transfer behavior in complex internal flow passages - Instrumentation for gas turbine research in short-duration facilities - Investigation of transonic inlet drag characteristics - Dynamic pressure fluctuations in the internozzle. Region of a twuin-jet nacelle - Temperature distortion generator for turboshaft engine testing - Results of a wind tunnel/flighht test program to compare afterbody/nozzle pressures on a 1/12 scale model and an F-15 aircraft - Application of technology to achieve value-added in-service support - Repairing commercial aircraft jet engine nacelle composite structures - Reliability assessment from small sample inspection data for gas turbine engine components - Failure modes and effects analysis method for new product introductions - Engine system field experience simulation program.
Tipo de ítem: Libro
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Aerospace Congress and Exposition (15 al 18 de octubre de 1984: Long Beach, California).

Design and experimental evaluation of propfan inlets - Engine inlet interaction with a prop-fan propulsion system - Stability and control results for advanced turboprop aft-mount installations - Aerodynamic test results for a wing-mounted turboprop propulsion installation - Advanced research instrumentation for aircraft turbomachinery - Acquisition of detailed heat transfer behavior in complex internal flow passages - Instrumentation for gas turbine research in short-duration facilities - Investigation of transonic inlet drag characteristics - Dynamic pressure fluctuations in the internozzle. Region of a twuin-jet nacelle - Temperature distortion generator for turboshaft engine testing - Results of a wind tunnel/flighht test program to compare afterbody/nozzle pressures on a 1/12 scale model and an F-15 aircraft - Application of technology to achieve value-added in-service support - Repairing commercial aircraft jet engine nacelle composite structures - Reliability assessment from small sample inspection data for gas turbine engine components - Failure modes and effects analysis method for new product introductions - Engine system field experience simulation program.

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