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A computational study of the wing–wing and wing–body interactions of a model insect

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An Erratum to this article was published on 11 November 2009

Abstract

The aerodynamic interaction between the contralateral wings and between the body and wings of a model insect are studied, by using the method of numerically solving the Navier–Stokes equations over moving overset grids, under typical hovering and forward flight conditions. Both the interaction between the contralateral wings and the interaction between the body and wings are very weak, e.g. at hovering, changes in aerodynamic forces of a wing due to the present of the other wing are less than 3% and changes in aerodynamic forces of the wings due to presence of the body are less than 2%. The reason for this is as following. During each down- or up-stroke, a wing produces a vortex ring, which induces a relatively large jet-like flow inside the ring but very small flow outside the ring. The vortex rings of the left and right wings are on the two sides of the body. Thus one wing is outside vortex ring of the other wing and the body is outside the vortex rings of the left and right wings, resulting in the weak interactions.

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Correspondence to Mao Sun.

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The project was supported by the National Natural Science Foundation of China(10732030) and the 111 Project (B 07009).

An erratum to this article can be found at http://dx.doi.org/10.1007/s10409-009-0315-x

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Yu, X., Sun, M. A computational study of the wing–wing and wing–body interactions of a model insect. Acta Mech Sin 25, 421–431 (2009). https://doi.org/10.1007/s10409-009-0266-2

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  • DOI: https://doi.org/10.1007/s10409-009-0266-2

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