Verwandte Artikel zu Theoretical and Experimental Study of Helicopter Icing...
Theoretical and Experimental Study of Helicopter Icing Scaling Methods: An Investigation of the Helicopter Ice Accretion Testing and Evaluation Tools - Softcover
Inhaltsangabe
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.
Die Inhaltsangabe kann sich auf eine andere Ausgabe dieses Titels beziehen.
Reseña del editor
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.
„Über diesen Titel“ kann sich auf eine andere Ausgabe dieses Titels beziehen.
EUR 120,19
EUR 28,88 für den Versand von Vereinigtes Königreich nach USA
Versandziele, Kosten & DauerNeu kaufen
Diesen Artikel anzeigen
EUR 59,00
EUR 23,00 für den Versand von Deutschland nach USA
Versandziele, Kosten & DauerSuchergebnisse für Theoretical and Experimental Study of Helicopter Icing...
Foto des Verkäufers
Theoretical and Experimental Study of Helicopter Icing Scaling Methods
Verlag:
LAP LAMBERT Academic Publishing Dez 2011, 2011
ISBN 10: 3846598291
ISBN 13: 9783846598290
Neu
Taschenbuch
Anbieter: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Deutschland
Verkäuferbewertung 5 von 5 Sternen
Taschenbuch. Zustand: 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. Bestandsnummer des Verkäufers 9783846598290
Anzahl: 2 verfügbar
Foto des Verkäufers
Theoretical and Experimental Study of Helicopter Icing Scaling Methods
Verlag:
LAP LAMBERT Academic Publishing, 2011
ISBN 10: 3846598291
ISBN 13: 9783846598290
Neu
Softcover
Anbieter: moluna, Greven, Deutschland
Verkäuferbewertung 5 von 5 Sternen
Zustand: 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. Bestandsnummer des Verkäufers 5502270
Anzahl: Mehr als 20 verfügbar
Foto des Verkäufers
Theoretical and Experimental Study of Helicopter Icing Scaling Methods
Verlag:
LAP LAMBERT Academic Publishing Dez 2011, 2011
ISBN 10: 3846598291
ISBN 13: 9783846598290
Neu
Taschenbuch
Anbieter: buchversandmimpf2000, Emtmannsberg, BAYE, Deutschland
Verkäuferbewertung 5 von 5 Sternen
Taschenbuch. Zustand: 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. Bestandsnummer des Verkäufers 9783846598290
Anzahl: 1 verfügbar
Foto des Verkäufers
Theoretical and Experimental Study of Helicopter Icing Scaling Methods : An Investigation of the Helicopter Ice Accretion Testing and Evaluation Tools
Verlag:
LAP LAMBERT Academic Publishing, 2011
ISBN 10: 3846598291
ISBN 13: 9783846598290
Neu
Taschenbuch
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Verkäuferbewertung 5 von 5 Sternen
Taschenbuch. Zustand: 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. Bestandsnummer des Verkäufers 9783846598290
Anzahl: 1 verfügbar
Beispielbild für diese ISBN
Theoretical and Experimental Study of Helicopter Icing Scaling Methods: An Investigation of the Helicopter Ice Accretion Testing and Evaluation Tools
Verlag:
LAP LAMBERT Academic Publishing, 2011
ISBN 10: 3846598291
ISBN 13: 9783846598290
Gebraucht
Paperback
Anbieter: Mispah books, Redhill, SURRE, Vereinigtes Königreich
Verkäuferbewertung 4 von 5 Sternen
Paperback. Zustand: Like New. Like New. book. Bestandsnummer des Verkäufers ERICA79638465982916
Anzahl: 1 verfügbar