Flight and wind tunnel investigation of the effects of Reynolds number on installed boattail drag at subsonic speeds
- 10 January 1973
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- A Turbojet Simulator for Mach Numbers up to 2.0Published by ASME International ,1972