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Research article

First published 2015-3

A coupled free-wake/panel method for rotor/fuselage/empennage aerodynamic interaction and helicopter trims

Yihua Cao, Shaojie Lv, Guozhi Li

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2011-9

Quad-Rotor Unmanned Aerial Vehicle Helicopter Modelling & Control

Yogianandh Naidoo, Riaan Stopforth, Glen Bright

International Journal of Advanced Robotic Systems

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Research article

First published 2015-6

Experimental investigation on the aerodynamic interaction between a helicopter and ground obstacles

G Gibertini, D Grassi, C Parolini [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2006-5

Modelling three-dimensional dynamic stall of helicopter blades using computational fluid dynamics and neural networks

A Spentzos, G Barakos, K Badcock [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2017-4

Numerical assessment of an L-shaped Gurney flap for load control

Valentina Motta, Alex Zanotti, Giuseppe Gibertini [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2019

A design methodology for quiet and long endurance MAV rotors

Ronan Serré, Hugo Fournier, Jean-Marc Moschetta

International Journal of Micro Air Vehicles

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Research article

First published 2023-9

Control-oriented meta-learning

Spencer M. Richards, Navid Azizan, Jean-Jacques Slotine [...]

The International Journal of Robotics Research

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Research article

First published 2014-9

Evidence of vortex-induced lift on a yawed wing in reverse flow

Vrishank Raghav, Michael Mayo, Rafael Lozano [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2015-3

Vortex flow hypothesis for a yawed rotor blade in reverse flow *

Michael Mayo, Vrishank Raghav, Narayanan Komerath

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2025-3

A method to optimal design the geometric parameters of a foldable flapping wing based on quasi-steady aerodynamics

Zhang Jingjing, Luo Jinglin, Wu Xuhang

Proceedings of the Institution of Mechanical Engineers,Part C: Journal of Mechanical Engineering Science

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