The LANN program - An experimental and theoretical study of steady and unsteady transonic airloads on a supercritical wing
- 12 July 1983
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- A hybrid field panel/finite difference method for 3-D potential unsteady transonic flow calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Improved Version of LTRAN2 for Unsteady Transonic Flow ComputationsAIAA Journal, 1980
- Numerical solution of three-dimensional unsteady transonic flow overswept wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Numerical calculation of transonic flow about swept wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972