COMPUTATIONAL STUDY –THRUST VECTOR CONTROL SUPERSONIC SECONDARY FLOW INJECTION

Ragul B; Anand kumar S; Dinesh kumar M

COMPUTATIONAL STUDY –THRUST VECTOR CONTROL SUPERSONIC SECONDARY FLOW INJECTION

Authors: Ragul B, Anand kumar S, Dinesh kumar M

Unique Paper ID: 149088
Volume: 6
Issue: 10
PageNo: 351-354

Keywords: No Keywords Found

Abstract:
This paper presents the Computational study of flow through the Rocket Nozzle in order to manoeuvre the Rocket by means of Supersonic Secondary Injection of Hot gases. Well-designed nozzles can accelerate these gases to speeds of thousands of meters per second. In addition to accelerating the gases, nozzles are often responsible for steering (or â€œvectoringâ€) the flow in order to control the rocketâ€™s direction of flight in supersonic speed.

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ISSN: 2349-6002
Volume: 6
Issue: 10
PageNo: 351-354

COMPUTATIONAL STUDY –THRUST VECTOR CONTROL SUPERSONIC SECONDARY FLOW INJECTION

Available:https://ijirt.org/Article?manuscript=149088

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UGC Approved
Journal no 47859

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