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@article{149088,
        author = {Ragul B and Anand kumar S and Dinesh kumar M},
        title = {COMPUTATIONAL STUDY –THRUST VECTOR CONTROL SUPERSONIC SECONDARY FLOW INJECTION},
        journal = {International Journal of Innovative Research in Technology},
        year = {},
        volume = {6},
        number = {10},
        pages = {351-354},
        issn = {2349-6002},
        url = {https://ijirt.org/article?manuscript=149088},
        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 “vectoring”) the flow in order to control the rocket’s direction of flight in supersonic speed.},
        keywords = {},
        month = {},
        }