论文信息 - Simulation of flow around blade section with one degree of freedom aeroelastic flap

Simulation of flow around blade section with one degree of freedom aeroelastic flap

In this paper, simulation is considered of flow around flapped rotor sections with a degree of freedom in the flap deflection angle. For steady state validation, comparisons one made of numerical results for the flow around a flapped wing with experimental data. Modelling of a blade section with an 1-DOF aeroelastic flap is also considered.

[1] P. P. Friedmann,et al. Adaptive Control of Aeroelastic Instabilities in Transonic Flow and Its Scaling , 1997 .

[2] Kevin W. Noonan,et al. Wind Tunnel Evaluation of a Model Helicopter Main-Rotor Blade With Slotted Airfoils at the Tip , 2001 .

[3] Friedrich K. Straub,et al. Rotors with Trailing Edge Flaps: Analysis and Comparison with Experimental Data , 1998 .

[4] Mark Woodgate,et al. CFD Requirements for Efficient Smart-Rotor Analysis , 2009 .

[5] George N. Barakos,et al. Computational aerodynamics of hovering helicopter rotors , 2012 .

[6] George N. Barakos,et al. Analysis and design of a Flap-Equipped Low-Twist Rotor for Hover , 2009 .

[7] Earl H. Dowell. A Modern Course in Aeroelasticity , 1999 .

[8] George N. Barakos,et al. A framework for CFD analysis of helicopter rotors in hover and forward flight , 2006 .