Accuracy of an unstructured-grid upwind-Euler algorithm for the ONERA M6 wing
- 1 June 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 28 (6) , 397-402
- https://doi.org/10.2514/3.46040
Abstract
No abstract availableKeywords
This publication has 15 references indexed in Scilit:
- Euler flutter analysis of airfoils using unstructured dynamic meshesJournal of Aircraft, 1990
- Unsteady Euler airfoil solutions using unstructured dynamic meshesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Finite element Euler computations in three dimensionsInternational Journal for Numerical Methods in Engineering, 1988
- Multigrid solution of the two-dimensional Euler equations on unstructured triangular meshesAIAA Journal, 1988
- Finite elements in CFD: What lies aheadInternational Journal for Numerical Methods in Engineering, 1987
- Successes and challenges in computational aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- An adaptive finite element scheme for the Euler and Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Computational methods for unsteady transonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Finite volume solution of the two-dimensional Euler equations on a regular triangular meshAIAA Journal, 1986
- Calculation of Inviscid Transonic Flow over a Complete AircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986