Helicopter Autorotation performances

Name: Helicopter Autorotation performances
Brand: VDM Verlag Dr. Müller
SKU: 9783639181838
Price: 303.95 RON
Availability: InStock

UAV Helicopter Using Rectangular and Quadratic Blades

Autor: Mohamed Sukri Mat Ali

Limbă:

Legare: Carte broșată

Editura: VDM Verlag Dr. Müller

Disponibilitate: La editor doar la comandă

Expediem în 17-27 zile

303.95 lei

This study is an evaluation of the possibility to reduce the risk of landing of an unmanned helicopt...

Informații despre carte

Autor

Mohamed Sukri Mat Ali

Limbă

engleză

Legare

Carte - Carte broșată

Publicat

2009

Pagini

124

EAN

9783639181838

Enbook ID

06826394

Editura

VDM Verlag Dr. Müller

Greutate

181

Dimensiuni

150 x 220 x 6

Descriere completă

This study is an evaluation of the possibility to reduce the risk of landing of an unmanned helicopter in an autorotation manoeuvre. Using a point mass model, the analysis was focused on the main rotor system as it gave the highest impact on helicopter's total power required. Comparison on the characteristics of the original rectangular blade and modified quadratic blade was analytically and experimentally performed. From this study, it was found that, by using modified quadratic blade the steady rate of descent of the point mass model can be reduced by two percent and zero collective pitch is the best collective pitch correction setting after engine failure. Additionally, to make a safe landing by using this quadratic blade, landing flare phase is also needed to be performed.

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Helicopter Autorotation performances

UAV Helicopter Using Rectangular and Quadratic Blades

Informații despre carte

Descriere completă

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