On the use of higher-order finite-difference schemes on curvilinear and deforming meshes
By Miguel R. Visbal, Datta V. Gaitonde. 2002
1,053 citations recorded by the source corpus.
Subfields: Atmospheric Science, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/43eb13763dd4e6ca3bc5b9eb01ac6c241e436ed5
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In Atmospheric Science
- D. Garmann
- Sanjiva K. Lele
- Daniel J. Bodony
- Yongsheng Lian
- Wei Shyy
- Pierre Sagaut
- Marc Terracol
- Guillaume Desquesnes
In Computational Mechanics
- Zhijian Wang
- Hung T. Huynh
- Sanjiva K. Lele
- Krzysztof J. Fidkowski
- Haiyang Gao
- Per-Olof Persson
- D. Garmann
- Xiaowen Wang
Citations in the corpus
- Current Status of Jet Noise Predictions Using Large-Eddy Simulation (2008, methodology): “In the case ofUBLandLBL, the tridiagonal scheme of Visbal and Gaitonde [58], with f 0:47 and f 0, is used.”
- Dynamics of revolving wings for various aspect ratios (2014, methodology): “The time-metric terms are evaluated employing the procedures described in detail by Visbal & Gaitonde (2002) to ensure that the geometric conservation law (GCL) is satisfied.”
- Numerical investigation of the tone noise mechanism over laminar airfoils (2007, methodology): “Finally, the curvilinear extension strategy proposed by Visbal & Gaitonde (2002) has been retained to handle complex geometries.”
- High‐order CFD methods: current status and perspective (2013, methodology): “Many methods were developed for structured meshes, for example, [3–8].”
- Derivation of high-order compact finite difference schemes for non-uniform grid using polynomial interpolation (2005, background): “Visbal and Gaitonde [7] have shown that application of high-order compact schemes to non-smooth and time varying grids using Jacobian transformation leads to spurious oscillations, unless a proper filtering scheme is used.”
- Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers (2012, background): “Visbal & Gaitonde (2002) developed very-high-order finite-difference schemes for the simulation of compressible flows on stretched, curvilinear, and deforming meshes.”
- Laminar-Turbulent Transition of a Low Reynolds Number Rigid or Flexible Airfoil (2006, methodology): “following formula used byVisbal andGaitonde [58] is adopted in our work:”