Design and Analysis of Jet Vane Thrust Vectoring Nozzle using CFD and Optimization of Nozzle Parameters

D  Daljit Majil  nbsp

doi:10.17485/ijst/2016/v9i39/100778

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Design and Analysis of Jet Vane Thrust Vectoring Nozzle using CFD and Optimization of Nozzle Parameters

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Indian Journal of Science and Technology

DOI: 10.17485/ijst/2016/v9i39/100778

Year: 2016, Volume: 9, Issue: 39, Pages: 1-6

Original Article

Design and Analysis of Jet Vane Thrust Vectoring Nozzle using CFD and Optimization of Nozzle Parameters

D. Daljit Majil^*

Aeronautical Engineering, Vel Tech Dr. RR and Dr. SR Technical University, Chennai - 600062, Tamil Nadu, India; [email protected]
*Author for correspondence
Daljit Majil
Aeronautical Engineering
Email: [email protected]

This work is licensed under a Creative Commons Attribution 4.0 International License.

Abstract

This paper is dealing with optimization of various nozzle parameters (C-D Nozzle) such as Radius of Throat; Divergent angle.2-D model of nozzle is designed in ANSYS 14.5 which is then analyzed with fluent software for exit velocity for various nozzle parameters at the different values. Taguchi design technique is used for optimization of nozzle parameters to get optimum nozzle parameters of jet vane Thrust vectoring nozzle is analyzed for two different operating conditions i.e. one is at standard atmospheric condition and another one is for outer space condition.