Calculation of steady and oscillating airfoil flow fields via the Navier Stokes equations
- 9 January 1984
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- A low mach number Euler formulation and application to time-iterative LBI schemesAIAA Journal, 1983
- Generalized Coordinate Forms of Governing Fluid Equations and Associated Geometrically Induced ErrorsAIAA Journal, 1982
- Dynamic Stall of an Oscillating Airfoil in Turbulent Flow Using Time Dependent Navier-Stokes SolverPublished by Springer Nature ,1981
- A Turbulent Flow Navier-Stokes Analysis for an Airfoil Oscillating in PitchPublished by Springer Nature ,1981
- On the structure and use of linearized block implicit schemesJournal of Computational Physics, 1980
- Geometric Conservation Law and Its Application to Flow Computations on Moving GridsAIAA Journal, 1979
- Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional GeometriesAIAA Journal, 1978
- Solution of the multidimensional compressible Navier-Stokes equations by a generalized implicit methodJournal of Computational Physics, 1977
- Starting vortex, separation bubbles and stall: a numerical study of laminar unsteady flow around an airfoilJournal of Fluid Mechanics, 1975
- Practical calculations of transitional boundary layersInternational Journal of Heat and Mass Transfer, 1973