Amanote Research

Amanote Research

    RegisterSign In

Flight Dynamics of an Articulated Rotor Helicopter With an External Slung Load

Journal of the American Helicopter Society
doi 10.4050/jahs.46.3
Full Text
Open PDF
Abstract

Available in full text

Date

January 1, 2001

Authors
Dario FusatoGiorgio GuglieriRoberto Celi
Publisher

American Helicopter Society


Related search

Mathematical Modeling of Helicopter Dynamics With an External Sling Load

International Journal of Engineering and Technology(UAE)
ArchitectureHardwareEngineeringChemical EngineeringBiotechnologyEnvironmental EngineeringComputer Science
2018English

Aerodynamic Load Estimation of Helicopter Rotor in Hovering Flight

Journal of Aeronautics & Aerospace Engineering
2015English

Swing Damping for Helicopter Slung Load Systems Using Delayed Feedback

2009English

Helicopter Stabilizer Optimization Considering Rotor Downwash in Forward-Flight

Aircraft Engineering and Aerospace Technology
Aerospace Engineering
2016English

Modeling of the Cooperative Slung-Load Transportation System With Multiple Quad-Rotor Unmanned Aerial Vehicles

2014English

An Inverse Aeroacoustic Problem With Aerodynamic Constraint for a Helicopter Rotor

2018English

Problems of an Aerodynamic Interference Between Helicopter Rotor Slipstream and an Elevated Heliport

Journal of KONES
2019English

Efficient Global Optimization of Helicopter Rotor Blades for Vibration Reduction in Forward Flight

2006English

Modeling a Synchronous Generator With an External Rotor at Constant Magnets

2019English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy