1. CFD analysis of a rocket nozzle with two inlets at Mach 2.1;Pandey KM;J Environ Res Dev,2013
2. CFD analysis of a rocket nozzle with four inlets at Mach 2.1;Pandey KM;Int J Chem Eng Appl,2010
3. CFD analysis of convergent‐divergent nozzle 1‐3;Satyanarayana G;Acta Tech Corviniensis Bull Eng,2013
4. CFD simulation analysis of two‐dimensional convergent‐divergent nozzle;Ramesh Kumar R;Int J Ambient Energy,2020
5. Design and analysis of a fuel injector of a liquid rocket engine;Thirupathi M;Int J Eng Adv Technol,2015