Theoretical and Experimental Study of Helicopter Icing Scaling Methods: An Investigation of the Helicopter Ice Accretion Testing and Evaluation Tools

ISBN 10: 3846598291 / ISBN 13: 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. N° de ref. de la librería

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Sinopsis: 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.

Biografía del autor: 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.

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Han, Yiqiang
Editorial: LAP Lambert Academic Publishing (2011)
ISBN 10: 3846598291 ISBN 13: 9783846598290
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Descripción LAP Lambert Academic Publishing, 2011. Estado de conservación: New. This item is printed on demand for shipment within 3 working days. Nº de ref. de la librería KP9783846598290

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Descripción LAP Lambert Academic Publishing, 2011. PAP. Estado de conservación: New. New Book. Delivered from our UK warehouse in 3 to 5 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. Nº de ref. de la librería LQ-9783846598290

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Descripción LAP Lambert Academic Publishing, 2011. PAP. Estado de conservación: New. New Book. Shipped from US within 10 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. Nº de ref. de la librería IQ-9783846598290

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Descripción LAP Lambert Academic Publishing, Germany, 2011. Paperback. Estado de conservación: New. Aufl.. 220 x 150 mm. Language: English . Brand New Book ***** Print on Demand *****.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. Nº de ref. de la librería AAV9783846598290

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Descripción LAP LAMBERT Academic Publishing. Paperback. Estado de conservación: New. Paperback. 160 pages. Dimensions: 8.7in. x 5.9in. x 0.4in.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. This item ships from multiple locations. Your book may arrive from Roseburg,OR, La Vergne,TN. Paperback. Nº de ref. de la librería 9783846598290

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Descripción Estado de conservación: Good. Theoretical and Experimental Study of Helicopter Icing Scaling Methods: An Investigation of the Helicopter Ice Accretion Testing and Evaluation Tools. Nº de ref. de la librería Grb3736592

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