2019
DOI: 10.1016/j.jfluidstructs.2019.102712
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Experimental investigation of fluid–structure interaction in a bird-like flapping wing

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Cited by 9 publications
(8 citation statements)
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References 29 publications
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“…Thus the mean is found to increase with a decrease in the panel chord length. Interestingly, Deshpande & Modani (2019) noted the trend of increased with an increase in flapping frequency for moderately flexible wing configurations. Thus the effect of an increase in frequency or a decrease in chord is seen to be the same, because the tangential velocity is a function of both the chord and frequency .…”
Section: Resultsmentioning
confidence: 99%
“…Thus the mean is found to increase with a decrease in the panel chord length. Interestingly, Deshpande & Modani (2019) noted the trend of increased with an increase in flapping frequency for moderately flexible wing configurations. Thus the effect of an increase in frequency or a decrease in chord is seen to be the same, because the tangential velocity is a function of both the chord and frequency .…”
Section: Resultsmentioning
confidence: 99%
“…Moreover, Deshpande et al evaluated the dynamics of four flapping wings made of different materials with different deformation capabilities through phase-lock 2D PIV measurements [133]. Their results suggested that the wing stiffness and deformation, especially the trailing edge deformation, played essential roles in thrust generation.…”
Section: Devices For Visualizing Wing Deformation Effectsmentioning
confidence: 99%
“…The above equation is used to obtain the aerodynamic force for a single wing and a given flapping frequency range. Number of wings N used as a multiplication factor to get the AF for the actual flapping-wing configuration during comparison (N = 2 for NAL flapper [23] and Golden snitch [37] and ; 4 for DelflyII [38]). In general, this component of AF was as a thrust force and the thrust generation in a flapping wing is considered analogous to that of a rotary wing where in the latter case, the thrust force varies with a square of propeller RPM.…”
Section: Validationmentioning
confidence: 99%