An improved orthogonal grid generation method for solving flows past highly cambered aerofoils with and without roughness elements
DOI10.1016/j.compfluid.2014.07.031zbMath1391.76263OpenAlexW2014639194MaRDI QIDQ1641606
Yogesh G. Bhumkar, Pramodkumar M. Bagade, Tapan K. Sengupta
Publication date: 19 June 2018
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.compfluid.2014.07.031
Navier-Stokes equationsbypass transitionroughness effectscambered aerofoilshybrid hyperbolic-elliptic orthogonal grid generation
General aerodynamics and subsonic flows (76G25) Mesh generation, refinement, and adaptive methods for the numerical solution of initial value and initial-boundary value problems involving PDEs (65M50)
Cites Work
- Unnamed Item
- Orthogonal grid generation of an irregular region using a local polynomial collocation method
- Space-time discretizing optimal DRP schemes for flow and wave propagation problems
- Spurious waves in discrete computation of wave phenomena and flow problems
- Analysis of anisotropy of numerical wave solutions by high accuracy finite difference methods
- Generation of orthogonal grids with control of spacing
- 2D nearly orthogonal mesh generation with controls on distortion function
- Orthogonal mapping
- Boundary-fitted coordinate systems for numerical solution of partial differential equations. A review
- Orthogonal mapping in two dimensions
- Application of Bubnov-Galerkin formulation to orthogonal grid generation
- Orthogonal grid generation in a 2D domain via the boundary integral technique
- Performance of under-resolved two-dimensional incompressible flow simulations. II
- Analysis of central and upwind compact schemes.
- Numerical prediction of unsteady vortex shedding for large leading-edge roughness.
- Performance of under-resolved two-dimensional incompressible flow simulations
- 2D orthogonal grid generation with boundary point distribution control
- Current grid generation strategies and future requirements in hypersonic vehicle design, analysis and testing
- Automatic structured mesh generation around two-dimensional bodies defined by polylines or polyC1 curves
- Analysis of stability and accuracy of finite-difference schemes on a skewed mesh
- An improved method for calculating flow past flapping and hovering airfoils
- High Accuracy Computing Methods
- Turbulence structure in a boundary layer with two-dimensional roughness
- Generation of Body-Fitted Coordinates Using Hyperbolic Partial Differential Equations
- Bi-CGSTAB: A Fast and Smoothly Converging Variant of Bi-CG for the Solution of Nonsymmetric Linear Systems
- Starting vortex, separation bubbles and stall: a numerical study of laminar unsteady flow around an airfoil
- Accelerated flow past a symmetric aerofoil: experiments and computations
- Nearly orthogonal two-dimensional grid generation with aspect ratio control
- On spurious vortical structures.
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