Response of active control on the flow field of the duct pressure at supersonic Mach numbers

• Main Authors: Ridwan, R, Chaudhary, Zakir Ilahi, Baig, Maugal Ahmed Ali, Suheel, J I, Khan, Sher Afghan, Faheem, Mohammed
• Format: Article
• Language: English; English
• Published: Elsevier Ltd Kidlington Corporate Office, Kidlington, United Kingdom 2022
• Subjects: TL780 Rockets
• Online Access: http://irep.iium.edu.my/96807/7/96807%20-%20Response%20of%20active%20control%20on%20flow%20field%20of%20the%20duct%20pressure%20at.pdf; http://irep.iium.edu.my/96807/13/96807_Response%20of%20active%20control%20on%20the%20flow%20field_SCOPUS.pdf; http://irep.iium.edu.my/96807/; https://www.journals.elsevier.com/materials-today-proceedings; https://doi.org/10.1016/j.matpr.2022.02.132
• Institution: Universiti Islam Antarabangsa Malaysia

In this study, experiments were conducted to control the base pressure and wall pressure in the wake at considerably high Mach numbers for a duct diameter of 25 mm. Tests were done at Mach 1.87 and 2.2. The Nozzle Pressure Ratios considered are 3 to 11 at different expansion levels. These experiment...