Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings
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- Type
- article
- Published
- 1991-06-24
- Cited by
- 1,792
- References
- 16
- OpenAlex
- https://openalex.org/W2314156868
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:124031409
Keywords
Airfoil, Multigrid method, Computer science, Aerodynamics, Aerospace engineering
References
- Three-dimensional unsteady Euler solutions for propfans and counter-rotating propfans in transonic flow
- Solution of the Euler equations for two dimensional transonic flow by a multigrid method
- Computation of rotor blade flows using the Euler equations
- A time-accurate multiple-grid algorithm
- On Central-Difference and Upwind Schemes
- Solutions Of The Navier-Stokes Equations For The Flow About A Rotor Blade
- Computation of unsteady transonic flows by the solution of Euler equations
- A Multiple-Grid Scheme for Solving the Euler Equations
- Computational methods for unsteady transonic flows
- Transonic flutter analysis using the Euler equations
- Stability on the imaginary axis andA-stability of linear multistep methods
- Calculation of Unsteady Wake/Rotor Interaction
- Navier-Stokes Simulations of Rotor/Stator Interaction Using Patched and Overlaid Grids
- Nonlinear aspects of the transonic aeroelastic stability problem
- Time Accurate Multigrid Solutions of the Navier-Stokes Equations
- Multigrid algorithms for compressible flow calculations
Cited by
- Algorithms for automatic feedback control of aerodynamic flows
- Validation of NASA rotor 67 with openFOAM's transonic density-based solver
- Aspects of the recursive projection method applied to flow calculations
- Investigation of the influence of the turbulent transition on transonic periodic flow
- A higher order numerical method for transonic flows
- Theoretical study and software design for the implementation of a numerical scheme based on the Dual Time Stepping in COSMO LM.
- Construction de modèles d'ordre réduit non-linéaires basés sur la décomposition orthogonale propre pour l'aéroélasticité
- BENEFIT STUDIES FOR ROTOR WITH ACTIVE TWIST CONTROL USING WEAK FLUID-STRUCTURE COUPLING
- Heat Transfer Modelling in Gas Turbine Stage
- Code to Code Comparison of Aircraft-Mode Tilt-RotorAerodynamics
- Discrete-Frequency Noise Prediction Using a Harmonic Balance Method
- A Two-Dimensional Multigrid-Driven Navier-Stokes Solver for Multiprocessor Architectures
- Analysis of a CROR Propulsion System at High Angle of Attack and at Low Speed Flight Conditions
- Integrated RANS-LES Computations of Turbomachinery Components: Generic Compressor/Diffuser
- Progress in Weak Fluid-Structure-Coupling for Multibladed Rotors in High-Speed forward Flight
- Numerical Study of Three Dimensional Low Magnetic Reynolds Number Hypersonic Magnetohydrodynamic Flows
- A dual-time implicit preconditioned Navier-Stokes method for solving 2D steady/unsteady laminar cavitating/noncavitating flows using a Barotropic model
- Impact of the unsteady aerothermal environment on the turbine blades temperature
- Ein blockstrukturiertes Verfahren zur Simulation der Umströmung komplexer Konfigurationen
- Realistic simulations of delta wing aerodynamics using novel CFD methods
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