Transonic kernel function method for unsteady flow calculations using a unified linear pressure panel procedure
- 12 May 1980
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- A transonic doublet lattice method for unsteady flow calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- A lifting surface theory based on an unsteady linearized transonic flow modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- An implicit shock-fitting scheme for unsteady transonic flow computationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- A simplified theory of oscillating airfoils in transonic flow - Review and extensionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- 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
- A perturbation method for transonic flows about oscillating airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- A finite difference method for the solution of the transonic flow around harmonically oscillating wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- The Oscillating Wedge in a Supersonic StreamJournal of the Aeronautical Sciences, 1949