Supercritical wing design using numerical optimization and comparisons with experimentto improve C-141 cruise performance
- 15 January 1979
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Aerodynamic Investigation of C-141 Leading Edge Modification for Cruise Drag Reduction. Volume 1.Published by Defense Technical Information Center (DTIC) ,1979
- Computational transonic flow about realistic aircraft configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Application of Numerical Optimization to the Design of Supercritical Airfoils without Drag-CreepPublished by SAE International ,1977
- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974