2010
DOI: 10.1016/j.jfluidstructs.2010.03.004
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Experimental investigation of the effect of chordwise flexibility on the aerodynamics of flapping wings in hovering flight

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Cited by 75 publications
(65 citation statements)
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“…Relatively few experimental works have been carried out in this field to explore more about the complex aerodynamic phenomena occurring during the flapping flight (Mazaheri and Ebrahimi, 2010a;Murphy, 2008;Muniappan et al, 2004;Muniappan et al, 2005;Aditya and Malolan, 2007). Such research would complement recent numerical studies (Isogai and Harino, 2007;Gogulapati et al, 2008;Fritz and Long, 2004;Willis et al, 2006) on flapping flight, and give an insight into the performance of membranous wings over the entire range of practical Reynolds numbers.…”
Section: Introductionmentioning
confidence: 94%
“…Relatively few experimental works have been carried out in this field to explore more about the complex aerodynamic phenomena occurring during the flapping flight (Mazaheri and Ebrahimi, 2010a;Murphy, 2008;Muniappan et al, 2004;Muniappan et al, 2005;Aditya and Malolan, 2007). Such research would complement recent numerical studies (Isogai and Harino, 2007;Gogulapati et al, 2008;Fritz and Long, 2004;Willis et al, 2006) on flapping flight, and give an insight into the performance of membranous wings over the entire range of practical Reynolds numbers.…”
Section: Introductionmentioning
confidence: 94%
“…Alternatively, tremendous progress was done in the field of aerodynamics and Kinematics [7][8][9][10][11][12][13][14][15][16]. Vincent [17] found that the material of insect wing was similar to composite materials, many other researchers also believed that the wing of natural insects are composite structures [18][19][20].…”
Section: Introductionmentioning
confidence: 99%
“…In general, studies available in the literature on flapping mechanical birds are categorized into experimental and theoretical. A designoriented model for the unsteady aerodynamics of a flapping wing has been developed using a modified strip theory approach, which considers vortex-wake effects for partial leading edge suction and post-stall behavior [7]. In order to model a micro-air flapping wing as a system of three rigid bodies with rigidly attached wings and using D'Alembert's principle extended to rigid bodies, equations of motion for micro-air flapping wings were proposed [8].…”
Section: Introductionmentioning
confidence: 99%