Conclusions and Recommendations

Kroll, Norbert; Bieler, H.; Deconinck, H.; Couaillier, Vincent; Ven, Harmen; Sørensen, Kaare

doi:10.1007/978-3-642-03707-8_34

Cited by 5 publications

(5 citation statements)

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“…Because of its simple geometric features, it is widely used for verification of turbulence models. It has been computed by researchers seeking validation of their numerical scheme or time-stepping method (Kalkote et al, 2018a;Swanson and Turkel, 1987;Kroll et al, 2010;Abgrall and De Santis, 2013;Kalkote et al, 2018b) for laminar flows and for fully turbulent flows (Assam et al, 2018;Ladson, 1988;Majewski et al, 2018).…”

Section: Naca 0012mentioning

confidence: 99%

Performance of the k-kL model for aerodynamics applications

Kalkote

Kumar

Assam

et al. 2019

HFF

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Purpose The purpose of this paper is to study the predictability of the recently proposed length scale-based two-equation k-kL model for external aerodynamic flows such as those also encountered in the high-lift devices. Design/methodology/approach The two-equation k-kL model solves the transport equations of turbulent kinetic energy (TKE) and the product of TKE and the integral length scale to obtain the effect of turbulence on the mean flow field. In theory, the use of governing equation for length scale (kL) along with the TKE promises applicability in a wide range of applications in both free-shear and wall-bounded flows with eddy-resolving capability. Findings The model is implemented in the in-house unstructured grid computational fluid dynamics solver to investigate its performance for airfoils in difficult-to-predict situations, including stalling and separation. The numerical findings show the good capability of the model in handling the complex flow physics in the external aerodynamic computations. Originality/value The model performance is studied for stationary turbulent external aerodynamic flows, using five different airfoils, including two multi-element airfoils in high-lift configurations which, in the knowledge of the authors, have not been simulated with k-kL model until now.

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Section: Naca 0012mentioning

confidence: 99%

Performance of the k-kL model for aerodynamics applications

Kalkote

Kumar

Assam

et al. 2019

HFF

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“…Spectral element methods, such as the discontinuous Galerkin (DG) method [3], the flux reconstruction method [4], and the spectral volume/difference methods [5], are intrinsically designed to achieve high order accuracy on unstructured grids. Among these methods, DG has drawn great attention [6], and still undergoes rapid development.…”

Section: Introductionmentioning

confidence: 99%

A data-driven shock capturing approach for discontinuous Galekin methods

Hesthaven

2022

Computers & Fluids

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“…The development of high-order numerical technologies for engineering analysis has been underway for many years now. For example, Discontinuous Galerkin methods (DGM) have been largely studied in the literature, initially in a theoretical context [3], and now from the application point of view [4]. In many contributions, it is shown that the accuracy of the method strongly depends on the accuracy of the geometrical discretization [5][6][7].…”

Section: Introductionmentioning

confidence: 99%