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Theoretical and Experimental Study of Helicopter Icing Scaling Methods: An Investigation of the Helicopter Ice Accretion Testing and Evaluation Tools - Brossura
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Flight into icing conditions introduces the risk of ice accretion to helicopter rotors. To understand and avoid the dangers related to rotor icing, test facilities such as the NASA Glenn Icing Research Tunnel have been developed. Due to the confined test section size of most current icing test facilities, an icing test on a full-chord helicopter rotor blade is not possible. To fulfill the research need of a novel full-scale-chord rotor icing test facility, the Adverse Environment Rotor Test Stand (AERTS) was designed and constructed at the Vertical Lift Research Center of Excellence, at the Pennsylvania State University. This book gives a comprehensive review of the current aircraft icing research. Ice accretion experiments were conducted to validate ice shape reproduction capabilities of this facility. Classical ice scaling methods were introduced and implemented to ensure experimental ice shape reproduction for varying chord-size blades. The validity of applying scaling laws to low-thrusting rotors was demonstrated. The comprehensive aircraft icing database provided in this book can be applied widely to the aircraft design and testing procedures.
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L'autore
Yiqiang Han is currently a PhD candidate at the Pennsylvania State University. He is a graduate research assistant at the Adverse Environment Rotor Test Stand (AERTS) facility. His research focuses on Aircraft Icing, specifically on helicopter icing, airfoil performance degradation evaluation, wind turbine icing, and blade coating evaluation.
Le informazioni nella sezione "Su questo libro" possono far riferimento a edizioni diverse di questo titolo.
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Theoretical and Experimental Study of Helicopter Icing Scaling Methods
Editore:
LAP LAMBERT Academic Publishing, 2011
ISBN 10: 3846598291
ISBN 13: 9783846598290
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Da: moluna, Greven, Germania
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Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Han YiqiangYiqiang Han is currently a PhD candidate at the Pennsylvania State University. He is a graduate research assistant at the Adverse Environment Rotor Test Stand (AERTS) facility. His research focuses on Aircraft Icing, speci. Codice articolo 5502270
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Theoretical and Experimental Study of Helicopter Icing Scaling Methods
Editore:
LAP LAMBERT Academic Publishing Dez 2011, 2011
ISBN 10: 3846598291
ISBN 13: 9783846598290
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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 -Flight into icing conditions introduces the risk of ice accretion to helicopter rotors. To understand and avoid the dangers related to rotor icing, test facilities such as the NASA Glenn Icing Research Tunnel have been developed. Due to the confined test section size of most current icing test facilities, an icing test on a full-chord helicopter rotor blade is not possible. To fulfill the research need of a novel full-scale-chord rotor icing test facility, the Adverse Environment Rotor Test Stand (AERTS) was designed and constructed at the Vertical Lift Research Center of Excellence, at the Pennsylvania State University. This book gives a comprehensive review of the current aircraft icing research. Ice accretion experiments were conducted to validate ice shape reproduction capabilities of this facility. Classical ice scaling methods were introduced and implemented to ensure experimental ice shape reproduction for varying chord-size blades. The validity of applying scaling laws to low-thrusting rotors was demonstrated. The comprehensive aircraft icing database provided in this book can be applied widely to the aircraft design and testing procedures. 160 pp. Englisch. Codice articolo 9783846598290
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Theoretical and Experimental Study of Helicopter Icing Scaling Methods : An Investigation of the Helicopter Ice Accretion Testing and Evaluation Tools
Editore:
LAP LAMBERT Academic Publishing, 2011
ISBN 10: 3846598291
ISBN 13: 9783846598290
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Da: AHA-BUCH GmbH, Einbeck, Germania
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Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Flight into icing conditions introduces the risk of ice accretion to helicopter rotors. To understand and avoid the dangers related to rotor icing, test facilities such as the NASA Glenn Icing Research Tunnel have been developed. Due to the confined test section size of most current icing test facilities, an icing test on a full-chord helicopter rotor blade is not possible. To fulfill the research need of a novel full-scale-chord rotor icing test facility, the Adverse Environment Rotor Test Stand (AERTS) was designed and constructed at the Vertical Lift Research Center of Excellence, at the Pennsylvania State University. This book gives a comprehensive review of the current aircraft icing research. Ice accretion experiments were conducted to validate ice shape reproduction capabilities of this facility. Classical ice scaling methods were introduced and implemented to ensure experimental ice shape reproduction for varying chord-size blades. The validity of applying scaling laws to low-thrusting rotors was demonstrated. The comprehensive aircraft icing database provided in this book can be applied widely to the aircraft design and testing procedures. Codice articolo 9783846598290
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Immagini fornite dal venditore
Theoretical and Experimental Study of Helicopter Icing Scaling Methods
Editore:
LAP LAMBERT Academic Publishing Dez 2011, 2011
ISBN 10: 3846598291
ISBN 13: 9783846598290
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Taschenbuch
Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
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Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Flight into icing conditions introduces the risk of ice accretion to helicopter rotors. To understand and avoid the dangers related to rotor icing, test facilities such as the NASA Glenn Icing Research Tunnel have been developed. Due to the confined test section size of most current icing test facilities, an icing test on a full-chord helicopter rotor blade is not possible. To fulfill the research need of a novel full-scale-chord rotor icing test facility, the Adverse Environment Rotor Test Stand (AERTS) was designed and constructed at the Vertical Lift Research Center of Excellence, at the Pennsylvania State University. This book gives a comprehensive review of the current aircraft icing research. Ice accretion experiments were conducted to validate ice shape reproduction capabilities of this facility. Classical ice scaling methods were introduced and implemented to ensure experimental ice shape reproduction for varying chord-size blades. The validity of applying scaling laws to low-thrusting rotors was demonstrated. The comprehensive aircraft icing database provided in this book can be applied widely to the aircraft design and testing procedures.Books on Demand GmbH, Überseering 33, 22297 Hamburg 160 pp. Englisch. Codice articolo 9783846598290
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Theoretical and Experimental Study of Helicopter Icing Scaling Methods: An Investigation of the Helicopter Ice Accretion Testing and Evaluation Tools
Editore:
LAP LAMBERT Academic Publishing, 2011
ISBN 10: 3846598291
ISBN 13: 9783846598290
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Paperback
Da: Mispah books, Redhill, SURRE, Regno Unito
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Paperback. Condizione: Like New. Like New. book. Codice articolo ERICA79638465982916
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