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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 - Livres de poche

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
Livre non disponible
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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 - Livres de poche

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
Livre non disponible
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Balaji Jayanth Venkatesh:
Design and Performance Evaluation of a Propeller - Livres de poche

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

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

2012, ISBN: 3847370111

ID: A19242468

Kartoniert / Broschiert, mit Schutzumschlag neu, [PU:LAP Lambert Academic Publishing]

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Détails sur le livre
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.

Informations détaillées sur le livre - Design and Performance Evaluation of a Propeller


EAN (ISBN-13): 9783847370116
ISBN (ISBN-10): 3847370111
Version reliée
Livre de poche
Date de parution: 2012
Editeur: LAP LAMBERT Academic Publishing

Livre dans la base de données depuis 06.08.2007 03:16:03
Livre trouvé récemment le 07.11.2017 12:54:52
ISBN/EAN: 3847370111

ISBN - Autres types d'écriture:
3-8473-7011-1, 978-3-8473-7011-6


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