Trailing edge flow control for the mitigation of dynamic stall effects

31st European Rotorcraft Forum

Volumn 2005, Issue , 2005, Pages

  Davis, Gregory L ^a   Feszty, Daniel ^a   Nitzsche, Fred ^a  

^a CARLETON UNIVERSITY   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; COMPUTER SIMULATION; DAMPING; FLIGHT DYNAMICS; HELICOPTER ROTORS; LINEAR EQUATIONS; MATHEMATICAL MODELS; TORSIONAL STRESS; VIBRATION CONTROL; VORTEX FLOW;

DYNAMIC STALL EFFECT; FLAP DEFLECTION; TRAILING EDGE FLOW CONTROL; VERTICAL BLADE REACTION FORCE;

COMPUTATIONAL FLUID DYNAMICS;

EID: 33746630250     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

1. Friedmann P.P., Vibration and Noise Reduction Using Actively Controlled Flaps-Their Evolution and Potential for Improving Rotorcraft Technology, paper no. IF-079, IFASD Conference, Munich, Germany, 2005.
2. Kloeppel V., Enenkl B. Rotor Blade Control by Active Helicopter Servo Flaps. Paper no. IF-158 IFASD Conference, Munich, Germany, 2005.
3. th Annual Forum, Montreal, Quebec, 2002.
4. Fulton M.V., Hover Testing of a Small-Scale Rotor with On-Blade Elevons. AHS Journal, Vol. 46, April 2001, pp. 96-106
5. th Decennial Specialist's Conference on Aeromechanics, San Fransisco. 2004, pp. 49-60
6. st European Rotorcraft Forum, Florence, Italy. 2005
7. Barakos G., Badcock K., Gagliardi A., CFD Simulation of Flow Control Devices for Helicopter Rotors, CEAS/KATnet Conference, Bremen, Germany, 2005
8. Nixon M.W., AHS Technical Committee Highlights: Dynamics 2003-2004. Vertiflite, Winter 2004, pp. 52-56
9. Splettstoesser W.R. et. al., The HELINOISE Aeroacoustic Rotor Test in the DNW - Test Documentation and Representative Results, DLR-Mitt. 93-09, DLR, Braunschweig, Germany, 1993.
10. 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, pp 17-25, January 2004.
11. NTUA Internal Report on the GAST code. Aerodynamics Laboratory, Department of Mechanical Engineering, National Technical University of Athens, Greece, 2005
12. rd ICAS Congress, Toronto. 2002
13. Opoku D.G., Nitzsche F., Acoustic Validation of a New Code Using Particle Wake Aerodynamics and Geometrically-Exact Beam Structural Dynamics. Aeronautical Journal, Vol 109, 2005, pp. 257-267
14. Badcock K.J., Richards B.E. and Woodgate M.A., Elements of Computational Fluid Dynamics on Block Structured Grids Using Implicit Solvers. Progress in Aerospace Sciences, Vol 36, 2000, pp. 351-392
15. Beaubien R.J., Nitzsche F., Feszty D., Frequency Domain Solution for Transonic Flutter Using Computational Fluid Dynamics. Paper no. IF-102, IFASD Conference, Munich, Germany, 2005.
16. Galbraith R., Gracey M., Gilmour R., Collected Data for Tests on a NACA 0012 Aerofoil. Volume II: Pressure Data from Oscillatory Tests, University of Glasgow, Aero Report 9208, Glasgow, Scotland, UK, Feb. 1992
17. Leishman J.G., Principles of Helicopter Aerodynamics, Cambridge University Press, 2002.