Numerical investigation on performance of convergent–divergent nozzle with multi‐inlet combustion chamber of a rocket engine

Author:

Bhaskar Arun1,Sahu Mithilesh K.1ORCID

Affiliation:

1. Department of Mechanical Engineering Gayatri Vidya Parishad College of Engineering (A) Visakhapatnam India

Publisher

Wiley

Subject

Fluid Flow and Transfer Processes,Condensed Matter Physics

Reference21 articles.

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

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