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Software for calculating the performance of a turboprop engine: Application to the DART 536-7R reactor - Brossura
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Thrusters play a crucial role in the evolution of aircraft through the different phases of flight. This has led manufacturers to improve engine power in order to bring more efficient products to market that are both quieter and less polluting.In our study, we have developed a calculation code to study the performance of a turboprop engine according to the real cycle and also in non-adaptive mode.The engine will have to operate in a wide range of conditions in terms of Mach number, altitude and rpm. The geometry will then impose, apart from adaptation, constraints which do not exist at the level of the calculation of the initial cycle.The DART 536-7R engine was used as a reference for the application of the developed code.
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Software for calculating the performance of a turboprop engine
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Software for calculating the performance of a turboprop engine Application to the DART 5367R reactor
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Software for calculating the performance of a turboprop engine Application to the DART 5367R reactor
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Software for calculating the performance of a turboprop engine: Application to the DART 536-7R reactor
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Software for calculating the performance of a turboprop engine: Application to the DART 536-7R reactor
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Software for calculating the performance of a turboprop engine
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Sciencia Scripts Jul 2020, 2020
ISBN 10: 6200946728
ISBN 13: 9786200946720
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Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germania
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Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Thrusters play a crucial role in the evolution of aircraft through the different phases of flight. This has led manufacturers to improve engine power in order to bring more efficient products to market that are both quieter and less polluting.In our study, we have developed a calculation code to study the performance of a turboprop engine according to the real cycle and also in non-adaptive mode.The engine will have to operate in a wide range of conditions in terms of Mach number, altitude and rpm. The geometry will then impose, apart from adaptation, constraints which do not exist at the level of the calculation of the initial cycle.The DART 536-7R engine was used as a reference for the application of the developed code. 108 pp. Englisch. Codice articolo 9786200946720
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Software for calculating the performance of a turboprop engine
Editore:
Sciencia Scripts Jul 2020, 2020
ISBN 10: 6200946728
ISBN 13: 9786200946720
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Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
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Taschenbuch. Condizione: Neu. Neuware -Thrusters play a crucial role in the evolution of aircraft through the different phases of flight. This has led manufacturers to improve engine power in order to bring more efficient products to market that are both quieter and less polluting.In our study, we have developed a calculation code to study the performance of a turboprop engine according to the real cycle and also in non-adaptive mode.The engine will have to operate in a wide range of conditions in terms of Mach number, altitude and rpm. The geometry will then impose, apart from adaptation, constraints which do not exist at the level of the calculation of the initial cycle.The DART 536-7R engine was used as a reference for the application of the developed code.Books on Demand GmbH, Überseering 33, 22297 Hamburg 108 pp. Englisch. Codice articolo 9786200946720
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Software for calculating the performance of a turboprop engine : Application to the DART 536-7R reactor
Print on DemandDa: AHA-BUCH GmbH, Einbeck, Germania
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Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Thrusters play a crucial role in the evolution of aircraft through the different phases of flight. This has led manufacturers to improve engine power in order to bring more efficient products to market that are both quieter and less polluting.In our study, we have developed a calculation code to study the performance of a turboprop engine according to the real cycle and also in non-adaptive mode.The engine will have to operate in a wide range of conditions in terms of Mach number, altitude and rpm. The geometry will then impose, apart from adaptation, constraints which do not exist at the level of the calculation of the initial cycle.The DART 536-7R engine was used as a reference for the application of the developed code. Codice articolo 9786200946720
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Software for calculating the performance of a turboprop engine: Application to the DART 536-7R reactor
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Software for calculating the performance of a turboprop engine
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