Librería: Ria Christie Collections, Uxbridge, Reino Unido
EUR 139,78
Cantidad disponible: Más de 20 disponibles
Añadir al carritoCondición: New. In.
Librería: GreatBookPrices, Columbia, MD, Estados Unidos de America
EUR 153,69
Cantidad disponible: 15 disponibles
Añadir al carritoCondición: As New. Unread book in perfect condition.
Librería: GreatBookPrices, Columbia, MD, Estados Unidos de America
EUR 168,63
Cantidad disponible: 15 disponibles
Añadir al carritoCondición: New.
Librería: moluna, Greven, Alemania
EUR 119,56
Cantidad disponible: Más de 20 disponibles
Añadir al carritoCondición: New.
Librería: Revaluation Books, Exeter, Reino Unido
EUR 191,94
Cantidad disponible: 2 disponibles
Añadir al carritoHardcover. Condición: Brand New. 99 pages. 9.25x6.25x0.50 inches. In Stock.
Idioma: Inglés
Publicado por Springer Nature Singapore, 2017
ISBN 10: 9811060975 ISBN 13: 9789811060977
Librería: AHA-BUCH GmbH, Einbeck, Alemania
EUR 145,40
Cantidad disponible: 2 disponibles
Añadir al carritoBuch. Condición: Neu. Druck auf Anfrage Neuware - Printed after ordering - The book addresses computational methods for solving the problem of vibration, response, loads and stability of a helicopter rotor blade modeled as a rotating beam with flap or out-of-plane bending. The focus is on explaining the implementation of the finite element method in the space and time domain for the free vibration, aeroelastic response and stability problems. The use of Floquet analysis for the aeroelastic stability analysis of rotor blades is also shown. The contents of the book will be useful to researchers in aerodynamics and applied mechanics, and will also serve well professionals working in the aerospace industry.
Librería: Brook Bookstore On Demand, Napoli, NA, Italia
EUR 110,26
Cantidad disponible: Más de 20 disponibles
Añadir al carritoCondición: new. Questo è un articolo print on demand.
Idioma: Inglés
Publicado por SPRINGER NATURE Okt 2017, 2017
ISBN 10: 9811060975 ISBN 13: 9789811060977
Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
EUR 139,09
Cantidad disponible: 2 disponibles
Añadir al carritoBuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The book addresses computational methods for solving the problem of vibration, response, loads and stability of a helicopter rotor blade modeled as a rotating beam with flap or out-of-plane bending. The focus is on explaining the implementation of the finite element method in the space and time domain for the free vibration, aeroelastic response and stability problems. The use of Floquet analysis for the aeroelastic stability analysis of rotor blades is also shown. The contents of the book will be useful to researchers in aerodynamics and applied mechanics, and will also serve well professionals working in the aerospace industry. 99 pp. Englisch.