Effect of Active Gurney Flaps on Overall Helicopter Flight Envelope

Aeronautical Journal - United Kingdom
doi 10.1017/aer.2016.57
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Cambridge University Press (CUP)

Related search

A Flight Envelope Expansion Study for the XH-51A Compound Helicopter

1969English

Performance Improvement of Variable Speed Rotors by Gurney Flaps

Aerospace Science and Technology
Aerospace Engineering
2018English

Computational Modeling of Gurney Flaps and Microtabs by POD Method

Energies
ControlElectronic EngineeringEnergy EngineeringRenewable EnergyEnergyFuel TechnologySustainabilityOptimizationElectricalPower Technologythe Environment
2018English

Performance Enhancement of Rotors in Hover Using Fixed Gurney Flaps

2017English

Effects of System Movement in Flight on Helicopter-Borne Magnetic Gradiometry

English

Aerodynamic Load Estimation of Helicopter Rotor in Hovering Flight

Journal of Aeronautics & Aerospace Engineering
2015English

Aeroacoustic Simulation of a Complete H145 Helicopter in Descent Flight

Journal of the American Helicopter Society
2016English

Helicopter Stabilizer Optimization Considering Rotor Downwash in Forward-Flight

Aircraft Engineering and Aerospace Technology
Aerospace Engineering
2016English

Damaged Airplane Trajectory Planning Based on Flight Envelope and Motion Primitives

Journal of Aircraft
Aerospace Engineering
2014English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy