Flow Control on Helicopter-Rotor Blades Via Active Gurney Flap

Wieńczysław Stalewski

doi:10.2478/tar-2018-0007

References

[1] Gardner A.D., Richter K., Rosemann H., Numerical Investigation of Air Jets for Dynamic Stall Control on the OA209 Airfoil, Proceedings of ERF 2010, Paris, 7-9 September 2010.
Search in Google Scholar Back to article
[2] Heine, B., Mulleners, K., Gardner, A., Mai, H., On the effects of leading edge vortex generators on an OA209 airfoil, ODAS2009, 2009.
Search in Google Scholar Back to article
[3] Feszty D., Gillies E.A., Vezza M., “Alleviation of Airfoil Dynamic Stall Moments via Trailing-Edge Flap Flow Control”, AIAA Journal, Vol. 42, No. 1 (2004), pp. 17-25.10.2514/1.853
Search in Google Scholar Back to article
[4] Wang, J.J., Li Y.C., Choi K-S., Gurney flap – Life enhancement, mechanisms and applications, Progress in Aerospace Sciences 44 (2008), pp. 22-47.10.1016/j.paerosci.2007.10.001
Search in Google Scholar Back to article
[5] Active Gurney Flap, European Patent Application No. 11250481.6, Applicant: Claverham Limited Bristol.
Search in Google Scholar Back to article
[6] ANSYS, Inc., ANSYS FLUENT User’s Guide. Release 15.0, November 2013. Available from: http://www.ansys.com.
Search in Google Scholar Back to article
[7] Kinzel M.P., Maughmer M.D., Duque E.P.N, Numerical Investigation on the Aerodynamics of Oscillating Airfoils with Deployable Gurney Flaps, AIAA Journal Vol.48, No.7, July 2010.10.2514/1.J050070
Search in Google Scholar Back to article
[8] Gibertini G., Zanotti A., New Technique Implementation in GVPM, Deliverable Report of Clean-Sky Project GUM, GUM/WP2/D2.3, July 2015.
Search in Google Scholar Back to article

Flow Control on Helicopter-Rotor Blades Via Active Gurney Flap

References

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