Boundary layer thickness effect on boattail drag
- 26 July 1976
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- The effect of Reynolds number on the boattail drag of two wing-body configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975