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Synopsis
The satisfactory performance of an aircraft depends on the good performance of its engine installation and aerodynamic design. However, the information describing the performance characteristics of an engine installed on an aircraft is, in most cases, restricted to the manufacturer or technology developer country. Some indicators of the performance condition of helicopters and their installed engine are the power output and the fuel consumed by the engine. The general objective of this study is to estimate the in-flight-helicopter-engine installed performance. For this purpose, the H-225M (Airbus Helicopters) is used as the example helicopter. The specific objectives reached in this study are: (i) determine the influential parameters in the engine performance installed at final platform (helicopter); (ii) develop an experiment to collect performance data during the flight; (iii) analyze the results according to Analysis of Variance (ANOVA); (iv) obtain a mathematical model to estimate power and fuel consumption and verify the capability of the model prediction.
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- PublisherLAP LAMBERT Academic Publishing
- Publication date2019
- ISBN 10 613991406X
- ISBN 13 9786139914067
- BindingPaperback
- LanguageEnglish
- Number of pages92
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Helicopter Engine Performance Determination Using Analysis of Variance
Published by
LAP LAMBERT Academic Publishing Jul 2019, 2019
ISBN 10: 613991406X
ISBN 13: 9786139914067
New
Taschenbuch
Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germany
Seller rating 5 out of 5 stars
Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The satisfactory performance of an aircraft depends on the good performance of its engine installation and aerodynamic design. However, the information describing the performance characteristics of an engine installed on an aircraft is, in most cases, restricted to the manufacturer or technology developer country. Some indicators of the performance condition of helicopters and their installed engine are the power output and the fuel consumed by the engine. The general objective of this study is to estimate the in-flight-helicopter-engine installed performance. For this purpose, the H-225M (Airbus Helicopters) is used as the example helicopter. The specific objectives reached in this study are: (i) determine the influential parameters in the engine performance installed at final platform (helicopter); (ii) develop an experiment to collect performance data during the flight; (iii) analyze the results according to Analysis of Variance (ANOVA); (iv) obtain a mathematical model to estimate power and fuel consumption and verify the capability of the model prediction. 92 pp. Englisch. Seller Inventory # 9786139914067
Quantity: 2 available
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Helicopter Engine Performance Determination Using Analysis of Variance
Published by
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 613991406X
ISBN 13: 9786139914067
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Softcover
Seller: Books Puddle, New York, NY, U.S.A.
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Helicopter Engine Performance Determination Using Analysis of Variance
Published by
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 613991406X
ISBN 13: 9786139914067
New
Taschenbuch
Seller: AHA-BUCH GmbH, Einbeck, Germany
Seller rating 5 out of 5 stars
Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The satisfactory performance of an aircraft depends on the good performance of its engine installation and aerodynamic design. However, the information describing the performance characteristics of an engine installed on an aircraft is, in most cases, restricted to the manufacturer or technology developer country. Some indicators of the performance condition of helicopters and their installed engine are the power output and the fuel consumed by the engine. The general objective of this study is to estimate the in-flight-helicopter-engine installed performance. For this purpose, the H-225M (Airbus Helicopters) is used as the example helicopter. The specific objectives reached in this study are: (i) determine the influential parameters in the engine performance installed at final platform (helicopter); (ii) develop an experiment to collect performance data during the flight; (iii) analyze the results according to Analysis of Variance (ANOVA); (iv) obtain a mathematical model to estimate power and fuel consumption and verify the capability of the model prediction. Seller Inventory # 9786139914067
Quantity: 1 available
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Helicopter Engine Performance Determination Using Analysis of Variance
Published by
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 613991406X
ISBN 13: 9786139914067
New
Softcover
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Helicopter Engine Performance Determination Using Analysis of Variance
Published by
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 613991406X
ISBN 13: 9786139914067
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Softcover
Seller: moluna, Greven, Germany
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Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Gomes AlexMore than 10 years professional experience in Flight Testing. Alex graduated as Rotary Wings Flight Test Engineer in Brazilian Air Force Flight Test School (EFEV) in 2008. MSc. in Aerodynamics, Gas Turbine and Statistics by. Seller Inventory # 385877071
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Helicopter Engine Performance Determination Using Analysis of Variance
Published by
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 613991406X
ISBN 13: 9786139914067
New
Softcover
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Condition: New. PRINT ON DEMAND. Seller Inventory # 18395825263
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Helicopter Engine Performance Determination Using Analysis of Variance
Published by
LAP LAMBERT Academic Publishing Jul 2019, 2019
ISBN 10: 613991406X
ISBN 13: 9786139914067
New
Taschenbuch
Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germany
Seller rating 5 out of 5 stars
Taschenbuch. Condition: Neu. Neuware -The satisfactory performance of an aircraft depends on the good performance of its engine installation and aerodynamic design. However, the information describing the performance characteristics of an engine installed on an aircraft is, in most cases, restricted to the manufacturer or technology developer country. Some indicators of the performance condition of helicopters and their installed engine are the power output and the fuel consumed by the engine. The general objective of this study is to estimate the in-flight-helicopter-engine installed performance. For this purpose, the H-225M (Airbus Helicopters) is used as the example helicopter. The specific objectives reached in this study are: (i) determine the influential parameters in the engine performance installed at final platform (helicopter); (ii) develop an experiment to collect performance data during the flight; (iii) analyze the results according to Analysis of Variance (ANOVA); (iv) obtain a mathematical model to estimate power and fuel consumption and verify the capability of the model prediction.Books on Demand GmbH, Überseering 33, 22297 Hamburg 92 pp. Englisch. Seller Inventory # 9786139914067
Quantity: 2 available
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Helicopter Engine Performance Determination Using Analysis of Variance
Published by
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 613991406X
ISBN 13: 9786139914067
New
Paperback
Seller: Revaluation Books, Exeter, United Kingdom
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Paperback. Condition: Brand New. 92 pages. 8.66x5.91x0.21 inches. In Stock. Seller Inventory # zk613991406X
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