Short CV: Kanmaniraja Radhakrishnan is a Postdoctoral Researcher in the Department of Aerospace Engineering at Inha University. His research focuses on rocket and gas turbine propulsion, combustion, gas dynamics, and multiphase flows. He has contributed to numerous high-impact publications in areas such as pintle injector technology for rocket engines and advanced heat transfer modeling. His expertise extends to both theoretical and computational analysis, including Lagrangian and CFD approaches applied to aerospace engineering challenges.
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