2020
DOI: 10.1007/s11802-020-4214-x
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Propulsion Performance of Spanwise Flexible Wing Using Unsteady Panel Method

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Cited by 2 publications
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“…68,69 However, in regards to their advantages, panel methods have the limitation of not being able to account for the shape of the wake and may only suitable for cases where pressure forces are dominant rather than viscous. 70 The development of potential singularity distribution on body and wake surface downstream of the wing is depicted in Figure 8. In order to use this approach, the geometry of the wake should be prescribed on the basis of experimental evidence.…”
Section: Numerical Modelsmentioning
confidence: 99%
“…68,69 However, in regards to their advantages, panel methods have the limitation of not being able to account for the shape of the wake and may only suitable for cases where pressure forces are dominant rather than viscous. 70 The development of potential singularity distribution on body and wake surface downstream of the wing is depicted in Figure 8. In order to use this approach, the geometry of the wake should be prescribed on the basis of experimental evidence.…”
Section: Numerical Modelsmentioning
confidence: 99%