Nozzle expansion level effect on a suddenly expanded flow

• Main Authors: Khan, Sher Afghan, Rathakrishnan, E.
• Format: Article
• Language: English
• Published: Walter de Gruyter 2006
• Subjects: TL Motor vehicles. Aeronautics. Astronautics; TL780 Rockets
• Online Access: http://irep.iium.edu.my/46701/1/khan_s_a_-_2006_-_nozzle_expansion.pdf; http://irep.iium.edu.my/46701/; http://www.degruyter.com/view/j/tjj.2006.23.4/tjj.2006.23.4.233/tjj.2006.23.4.233.xml
• Institution: Universiti Islam Antarabangsa Malaysia

This investigation focuses attention on the effectiveness of active control in the form of micro-jets, located at the base region of a suddenly expanded axi-symmetric ducts, to control the base pressure. The experiments were conducted for Mach numbers 1.25, 1.3, 1.48, 1.6, 1.8, 2.0, 2.5, and 3.0 at...