Aerodynamic shape optimization of rotor airfoils undergoing unsteady motion

17th Applied Aerodynamics Conference

Volumn , Issue , 1999, Pages 71-79

  Yee, Kwanjung ^a   Kim, Yushin ^a   Lee, Dong Ho ^a  

^a Seoul National University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRFOILS; DESIGN; INVERSE PROBLEMS; PRODUCT DESIGN; SURFACE PROPERTIES;

AERODYNAMIC SHAPE OPTIMIZATION; DESIGN PROCEDURE; INVERSE DESIGNS; OBJECTIVE FUNCTIONS; OVERALL CHARACTERISTICS; RESPONSE SURFACE METHODOLOGY; RESPONSE SURFACE MODELS; WEIGHTING FUNCTIONS;

SHAPE OPTIMIZATION;

EID: 84964299709     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

1. P.G. Wilbey, “The Development of Rotor Airfoil Testing in the UK - The Creation of a Capability to Exploit a Design Opportunity”, 22nd European Rotorcraft Forum, Brighton, UK, pp.18.1-18.11, 1996
2. W.J. McCroskey, K.W. McAlister, L.W. Carr, S.L. Pucci, O. Lambert, and R.F. Indergrand, “Dynamic Stall on Advanced Airfoil Sections”, Journal of American Helicopter Society,.Vol.26, No.3, pp.40-50, 1981
3. J. Liiva and F.J. Davenport, “Dynamic Stall of Airfoil Sections for High-Speed Rotors”, Journal of American Helicopter Society, Vol.14, No.2, pp.26-33, 1969
4. B. Gustafton, “The Application of Airfoil studies to Helicopter Rotor-Design”, NACA TN No. 1812, 1949.
5. X-S Stivere Jr. and F. J. Rice Jr., “Aerodynamic Characteristics of Four NACA Airfoil. Sections Designed for Helicopter Rotor Blades”, NACA RB No. L5K02, 1946.
6. L.D. Kemp, “An Analytical Study-for Design of Advanceda Rotor Airfoils” NASA CR, 112, 297, 1973
7. D. W. Fanjoy, and W. A. Crossley, “Aerodynamic Shape Design for Rotor Airfoils via Genetic Algorithm” American Helicopter-Society 53rd Annual Forum, 1997.
8. F. Tapia, L.N. Sankar and D.P. Schrage, “An Inverse Aerodynamic Design Method for Rotor Blades in Forward Flight”; American Helicopter Society, 51st Annual Forum, 1995.
9. A.A. Hassan and B.D. Charles,. “Airfoil Design for Helicopter, Rotor Blades - A Three-Dimensional. Approach”, American Helicopter Society 50th Annual Forum, 1994
10. J.C. Narramore, J.B. Nalone and R. Vermeland, “Application of a New Navier-Stokes Inverse Method to the Design of Advanced Airfoils”, American Helicopter Society 46th Annual Forum, pp. 1089-1098, 1990
11. Y.H. Yu, S. Lee, K.W. McAlister, C. Tung, and C.U. Wang, “Dynamic Stall Control for Advanced Rotorcraft Application”, AIAA Journal, Vol. 33, No.2, pp.289-295, 1995
12. S. Burgee, A.A. Guinta, V. Balalbanov, B. Grossman, W.H. Mason, R. Narducci, R.T. Haftka, and L.T. Watson, “A Coarse-Grained Parallel Variable-Complexity Multidisciplinary Optimization Paradigm”, The International Journal of Supercomputer Applications and High Performance Computing, Vol. 10, No.4, pp. 269-299, 1996
13. D. Favier, A. Agnes, C. Barbi, and C. Maresca, “Combined Translation/Pitch Motion: A New Airfoil Dynamic Stall Simulation”, Journal of Aircraft, Vol.25, No.9, pp.805-814, 1988.
14. D. Favier, C. Maresca, and J. Rebont, “Dynamic Stall due to Fluctuations of Velocity and Incidence”, AIAA Journal, Vol.20, pp.865-871, 1982.
15. B.S. Baldwin and H. Lomax, “Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows”, AIAA paper, No.78-0257, 1978.
16. R.H. Myers, and D.C. Montgomery, Response Surface Methodology: Process and Product Optimization Using Designed Experiments, John Wiley & Sons, 1995.
17. J. Sobieszczanski-Sobieski, and R.T Haftka, “Multidisciplinary Aerospace Design Optimization: Survey of Recent Developtment”, AIAA Paper, No. 96-0711, 1996.
18. G. Venter, R.T. Haftka, and J.H. Starnes Jr., “Construction of Response Surfaces for Design Optimization Applications”, AIAA-96-4040-CP 1996
19. A.A. Guinta, “Aircraft Multidisciplinary Design Optimization Using Design of Experimental Theory and Response, Surface Modeling Methods”, Ph. D. Dissertation, Department of Aerospace Engineering, Virginia Polytechnic Institute and State University; Blacksburg, VA, 1997.
20. K. Yee, D.H.- Lee and S. Lee, “Unsteady Flowfield and Noise Propagation due to Transonic Airfoil-Airfoil Interaction”, AIAA. Journal, Vol. 36, No.5, pp.791-798, 1998.
21. I.H. Abbott and A.E. vonDoenhoff, Theory of Wing Sections, Dover Publications, Inc., New York, NY, 1959.
22. R.W. Prouty, Helicopter Performance Stability, and Control, PWS Publishers, 1986