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Design and Performance Evaluation of a Propeller - Balaji Jayanth Venkatesh
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Design and Performance Evaluation of a Propeller - neues Buch

ISBN: 9783847370116

ID: 377cd591c693f5d367a0e952b3453058

Design and Performance Evaluation of a Propeller for Micro-Air Vehicle Application The selection of small-diameter propellers for Micro-Air Vehicle (MAV) applications are usually carried out arbitrarily due to non-existence of performance data. The presence of vast performance data for larger propellers cannot be applied to these small-diameter propellers that operate at low Reynolds numbers, and the aerodynamic performance data at these low Reynolds numbers seldom exists. Analytical method such as momentum-blade element theory together with computational methods such as CFD can be relied upon to design and optimise the performance of propellers of any class. In the current work, the design and performance evaluation of a propeller applicable to a MAV is carried out for a given thrust of 1 N, diameter of 120 mm and speed of 10,000 rpm. The design was based on one-dimensional momentum theory. Design modifications were done by varying the blade setting angle at 75% radius to enhance the performance of the propeller. As a result, the maximum efficiency was obtained for a blade setting angle of 40°. Experimental data available in the literature were used to validate the CFD solution procedure applied to predict the performance characteristics of the propeller. Bücher / Fremdsprachige Bücher / Englische Bücher 978-3-8473-7011-6, LAP Lambert Academic Publishing

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Design and Performance Evaluation of a Propeller - Balaji Jayanth Venkatesh
Vergriffenes Buch, derzeit bei uns nicht verfügbar.
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Balaji Jayanth Venkatesh:
Design and Performance Evaluation of a Propeller - neues Buch

ISBN: 9783847370116

ID: 158018436

The selection of small-diameter propellers for Micro-Air Vehicle (MAV) applications are usually carried out arbitrarily due to non-existence of performance data. The presence of vast performance data for larger propellers cannot be applied to these small-diameter propellers that operate at low Reynolds numbers, and the aerodynamic performance data at these low Reynolds numbers seldom exists. Analytical method such as momentum-blade element theory together with computational methods such as CFD can be relied upon to design and optimise the performance of propellers of any class. In the current work, the design and performance evaluation of a propeller applicable to a MAV is carried out for a given thrust of 1 N, diameter of 120 mm and speed of 10,000 rpm. The design was based on one-dimensional momentum theory. Design modifications were done by varying the blade setting angle at 75% radius to enhance the performance of the propeller. As a result, the maximum efficiency was obtained for a blade setting angle of 40°. Experimental data available in the literature were used to validate the CFD solution procedure applied to predict the performance characteristics of the propeller. Design and Performance Evaluation of a Propeller for Micro-Air Vehicle Application Buch (fremdspr.) Bücher>Fremdsprachige Bücher>Englische Bücher, LAP Lambert Academic Publishing

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Design and Performance Evaluation of a Propeller - Balaji Jayanth Venkatesh
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Balaji Jayanth Venkatesh:
Design and Performance Evaluation of a Propeller - Taschenbuch

2012, ISBN: 3847370111

ID: 10409445645

[EAN: 9783847370116], Neubuch, [PU: LAP Lambert Academic Publishing Feb 2012], This item is printed on demand - Print on Demand Titel. Neuware - The selection of small-diameter propellers for Micro-Air Vehicle (MAV) applications are usually carried out arbitrarily due to non-existence of performance data. The presence of vast performance data for larger propellers cannot be applied to these small-diameter propellers that operate at low Reynolds numbers, and the aerodynamic performance data at these low Reynolds numbers seldom exists. Analytical method such as momentum-blade element theory together with computational methods such as CFD can be relied upon to design and optimise the performance of propellers of any class. In the current work, the design and performance evaluation of a propeller applicable to a MAV is carried out for a given thrust of 1 N, diameter of 120 mm and speed of 10,000 rpm. The design was based on one-dimensional momentum theory. Design modifications were done by varying the blade setting angle at 75% radius to enhance the performance of the propeller. As a result, the maximum efficiency was obtained for a blade setting angle of 40°. Experimental data available in the literature were used to validate the CFD solution procedure applied to predict the performance characteristics of the propeller. 76 pp. Englisch

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(*) Derzeit vergriffen bedeutet, dass dieser Titel momentan auf keiner der angeschlossenen Plattform verfügbar ist.
Design and Performance Evaluation of a Propeller - Balaji Jayanth Venkatesh
Vergriffenes Buch, derzeit bei uns nicht verfügbar.
(*)
Balaji Jayanth Venkatesh:
Design and Performance Evaluation of a Propeller - Taschenbuch

2012, ISBN: 3847370111

ID: 10409445645

[EAN: 9783847370116], Neubuch, [PU: LAP Lambert Academic Publishing Feb 2012], This item is printed on demand - Print on Demand Neuware - The selection of small-diameter propellers for Micro-Air Vehicle (MAV) applications are usually carried out arbitrarily due to non-existence of performance data. The presence of vast performance data for larger propellers cannot be applied to these small-diameter propellers that operate at low Reynolds numbers, and the aerodynamic performance data at these low Reynolds numbers seldom exists. Analytical method such as momentum-blade element theory together with computational methods such as CFD can be relied upon to design and optimise the performance of propellers of any class. In the current work, the design and performance evaluation of a propeller applicable to a MAV is carried out for a given thrust of 1 N, diameter of 120 mm and speed of 10,000 rpm. The design was based on one-dimensional momentum theory. Design modifications were done by varying the blade setting angle at 75% radius to enhance the performance of the propeller. As a result, the maximum efficiency was obtained for a blade setting angle of 40°. Experimental data available in the literature were used to validate the CFD solution procedure applied to predict the performance characteristics of the propeller. 76 pp. Englisch

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(*) Derzeit vergriffen bedeutet, dass dieser Titel momentan auf keiner der angeschlossenen Plattform verfügbar ist.
Design and Performance Evaluation of a Propeller - Balaji Jayanth Venkatesh
Vergriffenes Buch, derzeit bei uns nicht verfügbar.
(*)
Balaji Jayanth Venkatesh:
Design and Performance Evaluation of a Propeller - neues Buch

ISBN: 9783847370116

ID: 95980c774733054ff218f27b52d4d2a0

The selection of small-diameter propellers for Micro-Air Vehicle (MAV) applications are usually carried out arbitrarily due to non-existence of performance data. The presence of vast performance data for larger propellers cannot be applied to these small-diameter propellers that operate at low Reynolds numbers, and the aerodynamic performance data at these low Reynolds numbers seldom exists. Analytical method such as momentum-blade element theory together with computational methods such as CFD can be relied upon to design and optimise the performance of propellers of any class. In the current work, the design and performance evaluation of a propeller applicable to a MAV is carried out for a given thrust of 1 N, diameter of 120 mm and speed of 10,000 rpm. The design was based on one-dimensional momentum theory. Design modifications were done by varying the blade setting angle at 75% radius to enhance the performance of the propeller. As a result, the maximum efficiency was obtained for a blade setting angle of 40°. Experimental data available in the literature were used to validate the CFD solution procedure applied to predict the performance characteristics of the propeller. Bücher / Naturwissenschaften, Medizin, Informatik & Technik / Technik / Maschinenbau

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Design and Performance Evaluation of a Propeller
Autor:

Venkatesh, Balaji Jayanth

Titel:

Design and Performance Evaluation of a Propeller

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Detailangaben zum Buch - Design and Performance Evaluation of a Propeller


EAN (ISBN-13): 9783847370116
ISBN (ISBN-10): 3847370111
Gebundene Ausgabe
Taschenbuch
Erscheinungsjahr: 2012
Herausgeber: LAP LAMBERT Academic Publishing

Buch in der Datenbank seit 06.08.2007 03:16:03
Buch zuletzt gefunden am 31.01.2017 20:05:42
ISBN/EAN: 9783847370116

ISBN - alternative Schreibweisen:
3-8473-7011-1, 978-3-8473-7011-6


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