Interaction of two-dimensional impulsively started airfoils

Wu, Fu-bing; Zeng, Nian-dong; Zhang, Liang; Wu, De-ming

doi:10.1007/bf02918638

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Cited by 3 publications

(1 citation statement)

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“…• Eq. N+1: unsteady Kutta condition [11], stating that the flow must leave the cylinder at the lower separation point…”

Section: A C C E P T E D Mmentioning

confidence: 99%

Simulation of the flow past a circular cylinder using an unsteady panel method

Ramos‐García

Sarlak

Andersen

et al. 2017

Applied Mathematical Modelling

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“…• Eq. N+1: unsteady Kutta condition [11], stating that the flow must leave the cylinder at the lower separation point…”

Section: A C C E P T E D Mmentioning

confidence: 99%

Simulation of the flow past a circular cylinder using an unsteady panel method

Ramos‐García

Sarlak

Andersen

et al. 2017

Applied Mathematical Modelling

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Application of an unsteady double wake panel method for aeroelastic rotor analysis

Ravishankara¹,

Boorsma²

2023

AIAA SCITECH 2023 Forum

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Unsteady Double Wake Model for the Simulation of Stalled Airfoils

Ramos‐García¹,

Cayron²,

Sørensen³

2015

JPEE

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In the present work, the recent developed Unsteady Double Wake Model, USDWM, is used to simulate separated flows past a wind turbine airfoil at high angles of attack. The solver is basically an unsteady two-dimensional panel method which uses the unsteady double wake technique to model flow separation and its dynamics. In this paper, the calculated integral forces have been successfully validated against wind tunnel measurements for the FFA-W3-211 airfoil. Furthermore, the computed highly unsteady flow field is analyzed in detail for a set of angles of attack ranging from light to deep stall conditions.

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Interaction of two-dimensional impulsively started airfoils

Cited by 3 publications

References 4 publications

Simulation of the flow past a circular cylinder using an unsteady panel method

Simulation of the flow past a circular cylinder using an unsteady panel method

Application of an unsteady double wake panel method for aeroelastic rotor analysis

Unsteady Double Wake Model for the Simulation of Stalled Airfoils

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