Short Communication: Application of WENO (Weighted Essentially Non-oscillatory) Approach to Navier–Stokes Computations-Reference-Cited by-同舟云学术

Short Communication: Application of WENO (Weighted Essentially Non-oscillatory) Approach to Navier–Stokes Computations

Published:2004-04 Issue:3 Volume:18 Page:289-293
ISSN:1061-8562
Container-title:International Journal of Computational Fluid Dynamics
language:en
Short-container-title:International Journal of Computational Fluid Dynamics

Author:

Epstein B.,Peigin S.

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics

Link

http://www.tandfonline.com/doi/pdf/10.1080/1061-8560310001621243

Reference9 articles.

1. Carr, M.P. and Palister, K.C. (1984) “Pressure distributions measured on research Wing M100 mounted on an axisymmetric body”,AGARD, AR-138

2. An Accurate ENO Driven Multigrid Method Applied to 3D Turbulent Transonic Flows

3. Accurate Multiblock Navier-Stokes Solver for Complex Aerodynamic Configurations

Cited by 11 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. High-Order WENO-based Semi-Implicit Projection Method for Incompressible Turbulent Flows: Development, Accuracy, and Reynolds Number Effects;International Journal of Computational Fluid Dynamics;2023-04-21

2. An optimized compact reconstruction weighted essentially non‐oscillatory scheme for advection problems;Numerical Methods for Partial Differential Equations;2020-12-12

3. OPTIMAL AERODYNAMIC DESIGN OF A WING-BODY CONFIGURATION FOR A WIDE-BODY LONG-RANGE AIRCRAFT;Vestnik Tomskogo gosudarstvennogo universiteta. Matematika i mekhanika;2019-02

4. INVESTIGATION OF THE STABILITY OF OPTIMAL AERODYNAMIC DESIGNING OF THE THREE-DIMENSIONAL WINGFUSELAGE LAYOUT FOR A WIDE-BODY LONG-RANGE AIRCRAFT WITH REGARD TO ITS INITIAL SHAPE;Vestnik Tomskogo gosudarstvennogo universiteta. Matematika i mekhanika;2019

5. The Stability of the Optimal Aerodynamic Design of an Isolated Three-Dimensional Wing to Its Initial Form;Technical Physics;2018-12