Analysis of base pressure control with ribs at Mach 1.2 using CFD method

Analysis of base pressure control with ribs at Mach 1.2 using CFD method

This paper discusses the control of base pressure by passive means, where the jet is issued from a converging nozzle at sonic Mach number under a favorable pressure gradient. The effect of employing annular ribs on the enlarged duct and its impact on the flow field, as the passive control mechanism...

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Bibliographic Details
Main Authors: Ahmad Fakhruddin, Ahmad ‘Afy, Mahboobali, Fharukh Ahmed Ghasi, Khan, Ambareen, Akhtar, Mohammad Nishat, Khan, Sher Afghan, Pathan, Khizar Ahmed
Format: Article
Language:English
Published: SEMARAK ILMU PUBLISHING 2024
Subjects:
TL780 Rockets
Online Access:http://irep.iium.edu.my/115466/7/115466_%20Analysis%20of%20base%20pressure.pdf
http://irep.iium.edu.my/115466/
https://semarakilmu.com.my/journals/index.php/fluid_mechanics_thermal_sciences/article/view/11538
https://doi.org/10.37934/arfmts.123.1.108143
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Institution: Universiti Islam Antarabangsa Malaysia
Language: English

Internet

http://irep.iium.edu.my/115466/7/115466_%20Analysis%20of%20base%20pressure.pdf
http://irep.iium.edu.my/115466/
https://semarakilmu.com.my/journals/index.php/fluid_mechanics_thermal_sciences/article/view/11538
https://doi.org/10.37934/arfmts.123.1.108143

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