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Design and Performance Evaluation of a Propeller: Design and Performance Evaluation of a Propeller for Micro-Air Vehicle Application - Balaji Jayanth Venkatesh
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Balaji Jayanth Venkatesh:
Design and Performance Evaluation of a Propeller: Design and Performance Evaluation of a Propeller for Micro-Air Vehicle Application - Taschenbuch

ISBN: 3847370111

[SR: 2837950], Taschenbuch, [EAN: 9783847370116], LAP LAMBERT Academic Publishing, LAP LAMBERT Academic Publishing, Book, [PU: LAP LAMBERT Academic Publishing], LAP LAMBERT Academic Publishing, 60448011, Ingenieurwesen & Technik, 60603011, Atomenergie, 60458011, Bauwesen, 60575011, Bioengineering, 60449011, Chemie für Ingenieure, 60508011, Computertechnik für Ingenieure, 60625011, Design für Ingenieure, 60516011, Elektrotechnik, 60628011, Energie, 60571011, Fahrzeugtechnik, 60652011, Forschung, 60543011, Industrie, Herstellung & Abläufe, 60565011, Luft- & Raumfahrt, 60636011, Management, 108498011, Marine, 60637011, Materialien, 60556011, Materialwissenschaft, 60580011, Mechanik, 60610011, Nachschlagewerke, 1320252031, Patente & Erfindungen, 60604011, Petroleum, Bergbau & Erde, 60651011, Stromanalagen, 60618011, Telekommunikation, 60447011, Architektur, Technik & Ingenieurswesen, 54071011, Genres, 52044011, Fremdsprachige Bücher, 56441011, Technologie, 56447011, Erneuerbare Energien, 56448011, Innovationen, 1320311031, Nachschlagewerke, 56444011, Nanotechnologie, 56449011, Philosophie der Technologie, 56445011, Risiken, 56446011, Sicherheit & Gesundheit, 273011011, Soziale Aspekte, 54518011, Technisches Denken & Schreiben, 56451011, Technologie & Gesellschaft, 56211011, Technologiegeschichte, 56442011, Zukunftsforschung, 56047011, Wissenschaft, 54071011, Genres, 52044011, Fremdsprachige Bücher

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Design and Performance Evaluation of a Propeller : Design and Performance Evaluation of a Propeller for Micro-Air Vehicle Application - Balaji Jayanth Venkatesh
Vergriffenes Buch, derzeit bei uns nicht verfügbar.
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Balaji Jayanth Venkatesh:
Design and Performance Evaluation of a Propeller : Design and Performance Evaluation of a Propeller for Micro-Air Vehicle Application - Taschenbuch

2012, ISBN: 3847370111

ID: 22517898699

[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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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

ISBN: 9783847370116

[ED: Taschenbuch], [PU: LAP Lambert Academic Publishing], 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., DE, [SC: 2.00], Neuware, gewerbliches Angebot, 222x154x14 mm, 76, [GW: 133g], PayPal, offene Rechnung, Banküberweisung, sofortueberweisung.de, Internationaler Versand

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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: 836846888

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 Design and Performance Evaluation of a Propeller for Micro-Air Vehicle Application - Venkatesh, Balaji Jayanth
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Design and Performance Evaluation of a Propeller Design and Performance Evaluation of a Propeller for Micro-Air Vehicle Application - neues Buch

2012, ISBN: 3847370111

ID: A19242468

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Design and Performance Evaluation of a Propeller

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.

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 07.11.2017 12:54:52
ISBN/EAN: 9783847370116

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


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