CFD analysis of compressible flows in a convergent-divergent nozzle

• Main Authors: Khan, Sher Afghan, Ibrahim, Omar Mohamed, Aabid, Abdul
• Format: Conference or Workshop Item
• Language: English; English; English
• Published: Elsevier Ltd 2021
• Subjects: TL780 Rockets
• Online Access: http://irep.iium.edu.my/92657/1/92657_CFD%20analysis%20of%20compressible.pdf; http://irep.iium.edu.my/92657/2/92657_CFD%20analysis%20of%20compressible_WoS.pdf; http://irep.iium.edu.my/92657/3/92657_CFD%20analysis%20of%20compressible_SCOPUS.pdf; http://irep.iium.edu.my/92657/; https://www.journals.elsevier.com/materials-today-proceedings; https://doi.org/10.1016/j.matpr.2021.03.074
• Institution: Universiti Islam Antarabangsa Malaysia

The nozzle is a mechanical device that uses pressure energy and fluid enthalpy to increase the outflow velocity and control fluid flow direction. To obtain the nozzle duct’s shock pattern, the flow inside the nozzle must be supersonic with a Mach number greater than one. Experimentally, the shock pa...