Access the full text.
Sign up today, get DeepDyve free for 14 days.
Loading next page...
/lp/springer-journals/assessment-of-a-high-order-high-resolution-esweno-p-scheme-for-avi-bvi-tVY1qFpxUO
References (36)
-
V. Venkatakrishnan (1995)
Convergence to steady state solutions of the Euler equations on unstructured grids with limitersJournal of Computational Physics, 118
-
GR Srinivasan (1986)
1569AIAA J, 24
-
S. Park, O. Kwon (2021)
Numerical Study of Effects of Fuselage and Facility Wall on PSP Rotor Performance in HoverInternational Journal of Aeronautical and Space Sciences, 23
-
Rafael Borges, M. Carmona, B. Costa, W. Don (2008)
An improved weighted essentially non-oscillatory scheme for hyperbolic conservation lawsJ. Comput. Phys., 227
-
F. Acker, Rafael Borges, B. Costa (2016)
An improved WENO-Z schemeJ. Comput. Phys., 313
-
A Thom (2010)
2313AIAA J, 48
-
A. Thom, K. Duraisamy (2010)
High-resolution simulations of parallel blade-vortex interactionsAIAA Journal, 48
-
K. Nakahashi (1999)
An Intergrid-Boundary Definition Method for Overset Unstructured Grid Approach -
Soogab Lee, D. Bershader (1994)
Head-on parallel blade-vortex interactionAIAA Journal, 32
-
S Lee (1994)
16AIAA J, 32
-
G. Vatistas, V. Kozel, W. Mih (1991)
A simpler model for concentrated vorticesExperiments in Fluids, 11
-
GS Jiang (1996)
202J Comput Phys, 126
-
N. Yamaleev, M. Carpenter (2009)
High-Order Energy Stable WENO Schemes -
author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law -
R Borges (2008)
3191J Comput Phys, 227
-
GW Jo (2002)
37J Korean Soc Aeronaut Space Sci, 30
-
AK Henrick (2005)
542J Comput Phys, 207
-
G. Srinivasan, W. Mccroskey, J. Baeder (1985)
Aerodynamics of two-dimensional blade-vortex interactionAIAA Journal, 24
-
S. Park, O. Kwon, S. Lee (2022)
Improved high-order high-resolution energy stable weighted essentially non-oscillatory plus scheme for shock/vortex problemsAIP Advances
-
M. Damodaran, D. Caughey (1988)
Finite-volume calculation of inviscid transonic airfoil-vortex interactionAIAA Journal, 26
-
H. Lee, O. Kwon (2013)
Assessment of a high-order discontinuous Galerkin method for vortex convection and wave propagation on unstructured meshesJournal of Mechanical Science and Technology, 27
-
Guang-Shan Jiang, Chi-Wang Shu (1996)
Efficient Implementation of Weighted ENO SchemesJournal of Computational Physics, 126
-
HD Lee (2013)
3331J Mech Sci Technol, 27
-
Springer Nature or its licensor holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s) -
(1998)
1998)Multilevel k-way partitioning schemes for irregular graphs -
M. Jung, J. Hwang, O. Kwon (2014)
Assessment of Rotor Aerodynamic Performances in Hover Using an Unstructured Mixed Mesh Method -
C. Kitaplioglu, F. Caradonna, M. McCluer (1999)
An Experimental Study of Parallel Blade-Vortex Interaction Aerodynamics and Acoustics Utilizing an Independently Generated Vortex -
PL Roe (1981)
Approximate Riemann solvers, parameter vectors and differenceJ Comput Phys, 43
-
P. Roe (1997)
Approximate Riemann Solvers, Parameter Vectors, and Difference SchemesJournal of Computational Physics, 135
-
XD Liu (1994)
200J Comput Phys, 115
-
Xu-Dong Liu, S. Osher, T. Chan (1994)
Weighted essentially non-oscillatory schemesJournal of Computational Physics, 115
-
(2009)
High-order stable ESWENO schemes. In: Paper presented at the 47th AIAA aerospace sciences meeting including the new horizons and aerospace -
Kyu-Won Jo, W. Oh, O. Kwon, I. Lee (2002)
Prediction of Aeroelastic Displacement Under Close BVI Using Unstructured Dynamic MeshesJournal of The Korean Society for Aeronautical & Space Sciences, 30
-
A. Henrick, T. Aslam, J. Powers (2005)
Mapped weighted essentially non-oscillatory schemes: Achieving optimal order near critical pointsJournal of Computational Physics, 207
-
Publisher's Note Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations -
M Damodaran (1988)
1346AIAA J, 26
- Publisher
- Springer Journals
- Copyright
- Copyright © The Author(s), under exclusive licence to The Korean Society for Aeronautical & Space Sciences 2022. corrected publication 2022. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law.
- ISSN
- 2093-274X
- eISSN
- 2093-2480
- DOI
- 10.1007/s42405-022-00525-9
- Publisher site
- See Article on Publisher Site
Abstract
In the present study, two- and three-dimensional blade-vortex interaction problems were assessed by employing a Reynolds-averaged Navier–Stokes computational fluid dynamics solver based on mixed meshes. The meshes consisted of an unstructured near-body region and a Cartesian off-body region. To capture vortices with high resolution, WENO family schemes were used for computing inviscid fluxes on the Cartesian meshes. For the unstructured meshes, Roe’s flux difference splitting scheme was employed to compute inviscid fluxes. The resolution of the WENO family schemes was compared in terms of pressure coefficient distributions. It was found that, compared to the existing WENO family schemes, the ESWENO-P scheme is more stable and consistently resolves the airfoil/blade-vortex interaction problems with higher resolution.
Journal
International Journal of Aeronautical and Space Sciences – Springer Journals
Published: Nov 1, 2022
Keywords: High-order scheme; High-resolution scheme; Airfoil/blade-vortex interaction problem