Name: Boom Vibration of Helicopter (en Inglés)
SKU: 57353643
Price: 55950.00 CLP
Availability: InStock
Author: Abdul Awal, Ziad Bin ; Bin Ammoo, Mohd Shariff
ISBN: 9786200114488

portada Boom Vibration of Helicopter (en Inglés)

Boom Vibration of Helicopter (en Inglés)

Formato

Libro Físico

Autor

Ziad Bin Abdul Awal

Mohd Shariff Bin Ammoo

Editorial

LAP Lambert Academic Publishing

Idioma

Inglés

N° páginas

Encuadernación

Tapa Blanda

Dimensiones

22.9x15.2x0.4 cm

Peso

0.12 kg.

ISBN13

9786200114488

Categorías

Tecnología y actividades del automóvil

Boom Vibration of Helicopter (en Inglés)

Ziad Bin Abdul Awal (Autor) · Mohd Shariff Bin Ammoo (Autor) · LAP Lambert Academic Publishing · Tapa Blanda

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Reseña del libro "Boom Vibration of Helicopter (en Inglés)"

Balancing remains a precarious aspect for any rotating component in terms of stability, control and safety. The helicopter tail rotor often yields pre-eminent frequency vibration due to its lofty operational speed. As a matter of fact, vibration remains one of the main trepidations as it can lead to structural failure and low handling quality owing to the yawing motion from the tail rotor. This is greatly dependent on the imbalance of the helicopter tail rotor which is predominantly caused by the uneven distribution of weight of the blades. Generally, imbalance is adjusted by weight, pitch control rod and trim tab. Furthermore, the rotor blade defects can also cause the rotor to go out of track. Therefore, tracking and balancing must be performed in order to ensure the blades are appropriately balanced and tracked. Along these lines, in order to manage the vibration, it is of the essence to understand the effect of tail rotor speed and blade pitching on boom vibration of a helicopter.