Nonlinear aeroelastic effects in flapping wing micro air vehicles

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn , Issue , 2008, Pages

  Gogulapati, A ^a,b   Friedmann, P P ^a,b   Shyy, W ^a,b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AERODYNAMICS; FLEXIBLE WINGS; LAGRANGE MULTIPLIERS; MICRO AIR VEHICLE (MAV); RIGID WINGS; STRUCTURAL DYNAMICS; VORTEX FLOW;

AERODYNAMIC MODELING; AEROELASTIC RESPONSE; FLAPPING WING MICRO AIR VEHICLE; FLEXIBLE DEFORMATION; NONLINEAR AEROELASTIC MODELING; NONLINEAR STRUCTURAL DYNAMICS; UNSTEADY AERODYNAMIC LOAD; UPDATED LAGRANGIAN METHOD;

AEROELASTICITY;

EID: 77957771815     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-1817     Document Type: Conference Paper

References (45)

1. Mueller, T. J., Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle. Applications, Vol. 195, Progress in Aeronautics and Astronautics, published by AIAA, 2001.
2. Pines, D. J. and Bohorquez, F., "Challenges Facing Future Micro-Air-Vehicle Development," Journal of Aircraft, Vol. 43, No. 2, March - April 2006, pp. 290-305.
3. Ellington, C. P., "The Aerodynamics of Hovering Insect Flight," Philosophical Transactions of the Royal Society of London B, Vol. 305, 1981, pp. 1-181.
4. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 2006, AIAA Paper Number 2006-500.
5. Shyy, W., Berg, M., and Ljungqvist, D., "Flapping and Flexible Wings for Biological and Micro Air Vehicles," Progress in Aerospace Sciences, Vol. 35, 1999, pp. 455 - 505.
6. Sane, S. P., "The Aerodynamics of Insect Flight," The Journal of Experimental Biology, Vol. 206, 2003, pp. 4191 - 4208.
7. Lian, Y., Shyy, W., Viieru, D., and Zhang, B., "Membrane Wing Aerodynamics for Micro Air Vehicles," Progress in Aerospace Sciences, Vol. 39, 2003, pp. 425 - 465.
8. Ansari, S. A., Zbikowski, R., and Knowles, K., "Aerodynamic Modelling of Insect-like Flapping Flight for Micro Air Vehicles," Progress in Aerospace Sciences, Vol. 42, 2006, pp. 129-172.
9. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 2008, AIAA Paper No. 2008-523.
10. Shyy, W., Lian, Y., Tang, J., Viieru, D., and Liu, H., Aerodynamics of Low Reynolds Number Flyers, Cambridge University Press, 2008.
11. Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., Aeroelasticity, Addison Wesley Co., 1955.
12. Ellington, C. P., van den Berg, C., Willmott, A. P., and Thomas, A. L. R., "Loading-Edge Vortices in Insect Flight," Nature, Vol. 384, 1996, pp. 626 - 630.
13. Birch, J. M., Dickson, W. B., and Dickinson, M. H., "Force Production and Flow Structure of the Leading Edge Vortex on Flapping Wings at High and Low Reynolds number," The Journal of Experimental Biology, Vol. 207, 2004, pp. 1063 - 1072.
14. Shyy, W. and Liu, H., "Flapping Wings and Aerodynamic Lift: The Role of Loading-Edge Vortices," AIAA Journal, Vol. 45, No. 12, 2007, pp. 2817 - 2819.
15. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Honolulu, Hawaii, April 2007, AIAA Paper Number 2007-1757.
16. Singh, B., Dynamics and Aeroelasticity of Hover Capable Flapping Wings: Experiments and Analysis, Ph.D. thesis, University of Maryland, College Park, 2006.
17. Azuma, A. and Okomoto, M., "Theoretical Study on Two-Dimensional Aerodynamic Characteristics of Unsteady Wings," Journal of Theoretical Biology, Vol. 40, May 2005, pp. 67 - 78.
18. Polhamus, E. C., "A Concept of the Vortex Lift of Sharp Edge Delta Wings Based on a Leading-Edge Suction Analogy," Nasa tn d-3767, 1966.
19. Smith, M. J., "Simulating Moth Wing Aerodynamics," AIAA Journal, Vol. 34, No. 7, 1996, pp. 1348 - 1355.
20. Young, J. and Lai, J. C. S., "Oscillation Frequency and Amplitude Effects on the Wake of a Plunging Airfoil," AIAA Journal, Vol. 42, No. 10, 2004, pp. 2042 - 2052.
21. Katz, J., "A Discrete Vortex Method for the Non-steady Separated Flow over an Airfoil," Journal of Fluid Mechanics, Vol. 102, 1981, pp. 315-328.
22. Ansari, S. A., Zbikowski, R., and Knowles, K., "Non-linear Unsteady Aerodynamic Model for Insect-like Flapping Wing in the Hover. Part 1: Methodology and Analysis," Proceedings of the I MECH E Part G Journal of Aerospace Engineering, Vol. 220, No. 2, 2006, pp. 61-83.
23. Ansari, S. A., Zbikowski, R., and Knowles, K., "Non-linear Unsteady Aerodynamic Model for Insect-like Flapping Wing in the Hover. Part 1: Implementation and Validation," Proceedings of the I MECH E Part G Journal of Aerospace Engineering, Vol. 220, No. 2, 2006, pp. 169-186.
24. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 2007, AIAA Paper Number 2007-129.
25. th AIAA Fluid Dynamics Conference and Exhibit, Miami, FL, June 2007, AIAA Paper Number 2007-4212.
26. Wootton, R. J., "Functional Morphology of Insect Wings," Annual Review of Entymology, Vol. 37, 1992, pp. 113 - 140.
27. Wootton, R. J., Herbert, R. C., Young, P. G., and Evans, K. E., "Approaches to Modeling of Insect Wings," Philosophical Transactions of the Royal Society of London B, Vol. 358, 2003, pp. 1577 - 1587.
28. Combes, S. A. and Daniel, T. L., "Flexural Stiffness in Insect Wings: I. Scaling and Influence of Wing Venation," The Journal of Experimental Biology, Vol. 206, 2003, pp. 2979 - 2987.
29. Combes, S. A. and Daniel, T. L., "Into Thin Air: Contributions of Aerodynamic and Inertial-Elastic Forces to Wing Bending in the Hawkmoth Manduca Sexta," The Journal of Experimental Biology, Vol. 206, 2003, pp. 2999 - 3006.
30. Daniel, T. L. and Combes, S. A., "Flexible Wings and Fins: Bonding by Inertial or Fluid-Dynamic Forces," Integrative and Comparative Biology, Vol. 42, 2002, pp. 1044 - 1049.
31. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Newport, Rhode Island, May 2006, pp. 184-196, AIAA Paper Number 2006-1662.
32. Azuma, A., Azuma, S., Watanabe, I., and Furuta, T., "Flight Mechanics of a Dragonfly," Journal of Experimental Biology, Vol. 116, 1985, pp. 79 - 107.
33. MSC. MARC, Volumes A - D, 2005.
34. Bauchau, O. A. and Trainelli, L., "The Vectorial Parametrization of Rotation," Nonlinear Dynamics, Vol. 32, No. 1, 2003, pp. 71 - 92.
35. Kane, T. R., Likins, P. W., and Levinson, D. A., Spacecraft Dynamics, Mc-Graw Hill Publications, 1983.
36. Baruh, H., Analytical Dynamics, Mc-Graw Hill Publications, 1999.
37. MSC. NASTRAN, Reference Manual, 2004.
38. Saffman, P. G., Vortex Dynamics, Cambridge University Press, 1992.
39. Abbott, I. H. and von Doenhoff, A. E., Theory of Wing Sections: Including a Summary of Airfoil Data, Dover Publications, 1959.
40. Bathe, K., Finite Element Procedures, Prentice-Hall Inc., 1996.
41. Belytschko, T., Liu, W. K., and Moran, B., Nonlinear Finite Elements for Continua and Structures, Wiley & Sons Ltd., 2001.
42. Bathe, K., Ramm, E., and Wilson, E. L., "Finite Element Formulations for Large Deformation Dynamic Analysis," International Journal for Numerical Methods in Engineering, Vol. 9, 1975, pp. 353 - 386.
43. Chung, J. and Hulbert, G. M., "A Family of Single-Step Houbolt Time Integration Algorithms for Structural Dynamics," Computational Methods in Applied Mechanics and Engineering, Vol. 118, 1994, pp. 1 - 11.
44. Peroomian, O., Chakravarthy, S., Palaniswamy, S., and Goldberg, U., "Convergence Acceleration for Unified-Grid Formulation Using Preconditioned Implicit Relaxation," Reno, NV, January 1998, AIAA Paper 98-0116.
45. Peroomian, O., Chakravarthy, S., and Goldberg, U., "A "Grid-Transparent" Methodology for CFD," Reno, NV, January 1997, AIAA Paper 97-0724.