Rotorcraft Retreating Blade Stall Control

doi 10.2514/6.2000-2475
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics

Related search

Actuator Saturation in Individual Blade Control of Rotorcraft

2012English

Dynamic Mode Decomposition of Rotorcraft Blade Tip Vortex in Hovering State

AIP Advances
NanotechnologyAstronomyPhysicsNanoscience
2020English

Alternate Blade Stall and Rotating Stall in Vaned Diffuser. 1st Report. Effects of Impeller/Diffuser Clearance.

Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
Condensed Matter PhysicsMechanical Engineering
2000English

Dynamic Stall Life Cycle on a Rotating Blade in Steady Forward Flight

Journal of the American Helicopter Society
2015English

Numerical Simulation of Rotating Stall in Axial Compressor Blade Rows and Stages

1986English

Model Predictive Control Scheme for Rotorcraft Inverse Simulation

2011English

Numerical Simulation of Surface Roughness Effects on Dynamic Stall of Wind Turbine Blade

Journal of Power and Energy Systems
2013English

Energy-Based Nonlinear Control for a Quadrotor Rotorcraft

2013English

Control of Compressible Dynamics Stall Using Microjets

2003English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy