Abstract
The paper investigates the role of streamwise slots applied to the boat-tail section of a supersonic projectile at Mach numbers from 1.36 to 1.83. The aerodynamic drag and surface pressures were measured in a supersonic indraft wind tunnel. Computations were performed at M = 1.36 and compared with the wind tunnel data.
Original language | English |
---|---|
Title of host publication | 13th International Conference on Applied Mechanics, Cairo, Egypt |
Publication status | Published - May 2008 |
Event | 13th International Conference on Applied Mechanics, Cairo, Egypt - Duration: 1 Jan 1824 → … |
Conference
Conference | 13th International Conference on Applied Mechanics, Cairo, Egypt |
---|---|
Period | 1/01/24 → … |