Advances in aerospace propulsion : SP-594 /
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 instru...
Guardado en:
Autor Corporativo: | |
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Formato: | Libro |
Lenguaje: | Inglés |
Publicado: |
Warrendale :
Society of Automotive Engineers,
1984.
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Materias: | |
Aporte de: | Registro referencial: Solicitar el recurso aquí |
LEADER | 01987cam#a22002413a#4500 | ||
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110 | |a Society of Automotive Egineers. |g SAE. |9 302090 | ||
245 | 1 | 0 | |a Advances in aerospace propulsion : |b SP-594 / |c Society of Automotive Engineers. |
260 | |a Warrendale : |b Society of Automotive Engineers, |c 1984. | ||
300 | |a 160 p. : |b il. | ||
500 | |a Aerospace Congress and Exposition (15 al 18 de octubre de 1984: Long Beach, California). | ||
520 | 2 | |a 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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650 | 4 | |a TURBINAS DE GAS |9 268300 | |
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