An implicit conservative algorithm for steady and unsteady three-dimensional transonic potential flows
- 22 June 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- An alternating-direction implicit algorithm for unsteady potential flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- A strongly implicit procedure for steady three-dimensional transonic potential flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Numerical solution of three-dimensional unsteady transonic flow overswept wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- A CONSERVATIVE IMPLICIT FINITE DIFFERENCE ALGORITHEM FOR THE UNSTEADY TRANSONIC FULL POTENTIAL EQUATIONPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- A panel method to determine loads on oscillating airfoils in transonic flow with embedded shock wavesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Implicit computations of unsteady transonic flow governed by the full-potential equation in conservation formPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Artificial Compressibility Methods for Numerical Solutions of Transonic Full Potential EquationAIAA Journal, 1979
- Supercritical wing design using numerical optimization and comparisons with experimentto improve C-141 cruise performancePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Implicit finite-difference computations of unsteady transonic flows about airfoils, including the treatment of irregular shock-wave motionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977