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3 publications

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    Analysis of Flow around Conical, Ogive Nose Cones in Hypersonic Space Shuttle

    By Murali K., Sabik Nainar A, Maheshwaran .

    Abstract: Hypersonic flow is a high Mach number regime used to distinguish flow fields, phenomena and problems appearing at flight speed far greater than the speed of sound. In high speed flows shock waves are formed during the flow. High speed flow have high energy level, thus dissipate large amount of heat, resulting in high temperatures, which may even burn the surface. The nose cone should be built with an outer …

    Published in Research & Reviews : Journal of Space Science & Technology · Vol. 4, Issue 1, 2015 · pp. 1–7 Read article

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    Advanced Ceramic Matrix Composites in Rocket Nozzle

    By Murali Kunashekaran, Sridhar Sudhahar M, Sabik Nainar A, Mohamed Kamil, Jaikumar D, Pragtheeshwaran .

    Abstract: In earlier days rocket nozzles were made up of monolithic ceramics, zirconium, and nimonic alloys. Though the materials have the capability to withstand enough temperature, they have the drawbacks such as manufacturing cost & time, strength to weight ratio.In order to cut the manufacturing cost & time, the strength to weight ratio and also to improve the capability to withstand high temperature, a composite material—C/SiC—shows enough required properties in the …

    Published in Journal of Thermal Engineering and Applications · Vol. 2, Issue 3, 2015 · pp. 32–40 Read article

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    Design and Analysis Versatile Thrust Vectoring Characteristics of A Military Turbojet Engine

    By Murali K., Sabik Nainar A, Sridhar Sudhkaran M.

    Abstract: This paper under the title of “Versatile thrust vectoring characteristics of a military turbojet engine" deals with the latest developments that exist and those which are proposed to be established in the field of VTOL (Vertical Take-Off and Landing) aeronautical engineering. The biggest problem that exists today in that field is that no aircraft can have both Vertical takeoff and Supersonic cruise on a same design. To overcome this, a …

    Published in Journal of Aerospace Engineering & Technology · Vol. 5, Issue 1, 2015 · pp. 37–46 Read article

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