Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56

• Main Authors: Bashir, Musavir, Baig, Maughal Ahmed Al, Ismail, Ahmad Faris, Khan, Sher Afghan
• Format: Article
• Language: English
• Published: IOSR journals 2016
• Subjects: TL Motor vehicles. Aeronautics. Astronautics; TL1 Motor vehicles
• Online Access: http://irep.iium.edu.my/54294/1/Musavir.pdf; http://irep.iium.edu.my/54294/; http://www.iosrjournals.org/

Airflow from convergent-divergent axisymmetric nozzles expanded into circular duct of higher area were studied experimentally, with the main focus on the flow development in the duct. The flow parameters considered in this investigation are the Mach number at the nozzle exit and the level of expansi...