Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers

• المؤلفون الرئيسيون: Afzal, Asif, Khan, Sher Afghan, Islam, Md. Tariqul, Jilte, R. D., Khan, Ambareen, Soudagar, Manzoore Elahi M
• التنسيق: مقال
• اللغة: English; English; English
• منشور في: AIP Publishing 2020
• الموضوعات: TL780 Rockets
• الوصول للمادة أونلاين: http://irep.iium.edu.my/83245/1/83245_Investigation%20and%20back-propagation%20modeling_ft.pdf; http://irep.iium.edu.my/83245/7/83245_Investigation%20and%20back-propagation%20modeling_SCOPUS.pdf; http://irep.iium.edu.my/83245/8/83245_Investigation%20and%20back-propagation%20modeling_WOS.pdf; http://irep.iium.edu.my/83245/; https://aip.scitation.org/doi/10.1063/5.0022015; https://doi.org/10.1063/5.0022015
• المؤسسة: Universiti Islam Antarabangsa Malaysia

The experimental analysis of base pressure in a high-speed compressible flow is carried out. The flow is made to expand abruptly from the nozzle into an enlarged duct at fifteen sonic and supersonic Mach numbers. The analysis is made for variation in the nozzle pressure ratio (NPR), length to diamet...