Determination of optimum camber distribution in rotating wings with deformable airfoils for vibration reduction and performance enhancement using surrogate modeling

36th European Rotorcraft Forum, ERF 2010

Volumn 2, Issue , 2010, Pages 931-940

  Kumar, Devesh ^a   Glaz, Bryan ^a   Mok, Jiwon ^a   Friedmann, Peretz P ^a   Cesnik, Carlos E S ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRFOILS; DEFORMATION; ROTORS;

AEROELASTIC MODELING; DEFLECTION PROFILES; DEFORMATION AMPLITUDE; DESIGN VARIABLES; OPTIMIZATION FRAMEWORK; PERFORMANCE ENHANCEMENTS; VIBRATION CHARACTERISTICS; VIBRATION REDUCTIONS;

CAMBERS;

EID: 84927597677     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (28)

1. DAR?A. Mission Adaptive Rotor. Http://wvw.dairia.mil/tto/orograms/rnar/Aug, 2009
2. C. E. S. Cesnik, S-J. Shin, and M. L. Wilbur. "Dynamic Response of Active Twist Rotor Blades." Smart Mat. And Struct., Vol. 10, 2001, pp. 62-76.
3. L. Liu, P. P. Friedmann, I. Kim, and D. S. Bernstein. "Rotor Performance Enhancement and Vibration Reduction in Presence of Dynamic Stall Using Actively Controlled Flaps." Journal of the American Helicopter Society, Vol. 53, No. 4, May, 2006, 2008, pp. 338-350.
4. J. N. Kudwa. "Overview of the DARPA Smart Wing Project" Journal of Intelligent Material Systems and Structures, Vol. 15, 2004, pp. 261-267.
5. S. Kota, J. Hetrick, O. Rüssel, D. Paul, E. Pendleton, P. Flick, and C. Tiimann. "Design and Application of Compliant Mechanisms for Morphing Aircraft Structures." Proceedings of SPIE, Vol. 5054, No. 24, 2003, pp. 24-33.
6. M. J. Santer and S. Pellegrino. "Topology Optimization of Adaptive Compliant Aircraft Wing Leading Edge." AIAA Structures, Structural Dynamics, and Materials Conference, Honolulu, Hawaii, April, 2007.
7. L. Saggere and S. Kota. "Static Shape Control of Smart Structures Using Compliant Mechnisms." AIAA Journal, Vol. 37, No. 5, 1999, pp. 572-578.
8. F. Gandhi and P. Anusonti-Inthra. "Skin Design Studies for Variable Camber Morphing Airfoils." Smart Materials and Struct., Vol. 17, 2008, pp. 1-8.
9. O. K. Rendinotìs, L. N. Wilson, D. C. Lagoudas, and M.M.Khan. "Development of a Shape-Memory-Alloy Actuated Biomimetic Hydrofoil." Journal of Intelligent Material Systems and Structures, Vol. 13, 2002, pp. 35-49.
10. J. D. Bartley-Cho, D. P. Wang, C. A. Martin, J. N. Kudva, and M. N. West. "Developement of High-rate, Adaptive Trailing Edge Control Surface for the Smart Wing Phase 2 Wind Tunnel Model " Journal of Intelligent Material Systems and Structures, Vol. 15, 2004, pp. 279-291.
11. P. Anusonti-Inthra, F. Gandhi, and M. Frecker. "Design of a Comformable Rotor Airfoil using Distributed Piezoelectric Actuation." Proceedings of ASME International Mechanical Engineering Congress, Washington, D.C, November 2003.
12. F. Gandhi, M. Frecker, and A. Nissly. "Design Optimization of a Controllable Camber Rotor Airfoil." AIAA J, Vol. 46, No. 1, 2008, pp. 142-153.
13. A. Forester, A. Sobester and A. Keane. Engineering Design via Surrogate Modelling. A Practical Guide, AIAA, 2008.
14. N. V. Queipo, R. T. Haftka, W. Shy, T. Goel, R. Vaidyanathan and P. K. Tucker. "Surrogate-based Analysis and Optimization." Progress in Aerospace Sciences, Vol. 41, 2005, pp. 1-28.
15. T. W. Simpson, A. J. Booker, D. Ghosh, A. A. Guinta, P. N. Koch, and R. Yang. "Approximate Methods in Multidisciplinary Analysis and Optimization: A Panel Discussion." Structural and Multidisciplinary Optimization, Vol. 27, No. 5, 2004, pp. 302-313.
16. J. Martin and T. Simpson. "Use of Kriging Models to Approximate Deterministic Computer Models." AIAA J, Vol. 43, No. 4, 2005, pp. 853-863.
17. J. Sacks, W. J. Welch, T. J. Mitchell, and H. P. Wynn. "Design and Analysis of Computer Experiments." Statistical Science, Vol. 4, No. 4, 1989, pp. 409-435.
18. S. N. Lophaven, H. B. Nielsen, and J. Sondergaard. "A Matlab Kriging Toolbox, version 2.0." Informatics and Mathematical Modeling, 2002.
19. D. R. Jones, M. Schonlau, and W. J. Welch. "Efficient Global Optimization of Epensive Black Box Functions." Journal of Global Optimization, Vol. 13, 1998, pp. 455-492.
20. B. Glaz, P. P. Friedmann, and L. Liu. "Helicopter Vibration Reduction Throughout the Entire Envelope Using Surrogate-based Optimization." Journal of American Helicopter Society, Vol. 54, No. 1, Jan 2009.
21. S. Thepvongs, C. E. S. Cesnik, R. Palacios, and D. A. Peters. "Finite-State Aeroelastic Modeling of Rotating Wings with Deformable Airfoils." American Helicopter Society 65th Annual Forum, 2008.
22. S. Thepvongs, J. R. Cook, C. E. S. Cesnik, and M. J. Smith. "Computational Aeroelastiçity of Rotating Wings with Deformable Airfoils." Proceedings of American Helicopter Soceity 65th Annual Forum, Grapevine, Texas, May, 2009, 2009.
23. R Palacios and C. E. S. Cesnik. "Geometrically Nonlinear Theory of Composite Beams with Deformable Cross Sections." AIAA Journal, Vol. 46, No. 2, 2008, pp. 439-450.
24. R. Palacios and C. E. S. Cesnik. "Low-Speed Aeroelastic Modeling of Very Flexible Slender Wings with Deformable Airfoils." AIAA Structures, Structural Dyamics and Materials Conference, Schaumburg, IL, April 2008.
25. R Palacios and C. E. S. Cesnik. "Cross-Sectional Analysis of Nonhomogenous Anisotropic Active Slender Structures." AIAA Journal, Vol. 43, No. 12, 5 July 2005, pp. 2624-2638.
26. D. A. Peters, M. A. Hsieh, and A. Torrero. "A State Space Airloads Theory for Flexible Airfoils." American Helicopter Society 63rd Annual Forum, Phoenix, AZ, May, 2006.
27. J. Murua, R. Palacios, and J. Peiro. "Camber Effects in the Dynamic Aeroelastiçity of Compliant Airfoils." International Forum on Aeroelastiçity and Structural Dynamics, Seattle, Washington, 2009.
28. M. L. Wilbur, J. William T. Yeager, and M. K. Sekula. "Further examination of the vibratory loads reduction results from the NASA/ARMY/MIT active twist rotor." American Helicopter Society 58th Annual Forum, Montreal, Canada, June, 2002.