Aerothermodynamic Design and Optimisation of Hypersonic Research Reentry Vehicle
International Journal of Science and Research (IJSR)

International Journal of Science and Research (IJSR)
www.ijsr.net | Most Trusted Research Journal Since Year 2012

ISSN: 2319-7064



Research Paper | Mechanical Engineering | India | Volume 3 Issue 7, July 2014

Aerothermodynamic Design and Optimisation of Hypersonic Research Reentry Vehicle

Manjunatha H, C. N. Nataraj

Among variety of design requirements reducing the aero heating problem is most crucial one. The hypersonic vehicle flying at hypersonic speed generates strong bow shock ahead of nose which is responsible for aero heating problem; the problem can be analyzed in two ways without spike and with spike. This investigation considers the mach 9.0 with analyzing the temperature, pressure, heat flux, and heat transfer co efficient over the body surface with two different predefined pressure conditions i.e.50 and 100 bar for without spike and with spike. Spike design replaces strong shock instead of weaker shocks at the nose and weaker shocks reduce the temperature at the vehicle. It is found that with spike yields better results than without spike vehicle. with different predefined pressure conditions. Model created in solid works, and meshing in Gambit 2.4.6 finally solution is by Fluent 6.3 solver.

Keywords: CFD, aero heating problem, spike, Heat flux q, heat transfer co-efficient ch

Edition: Volume 3 Issue 7, July 2014

Pages: 1234 - 1238

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How to Cite this Article?

Manjunatha H, C. N. Nataraj, "Aerothermodynamic Design and Optimisation of Hypersonic Research Reentry Vehicle", International Journal of Science and Research (IJSR), https://www.ijsr.net/search_index_results_paperid.php?id=20141252, Volume 3 Issue 7, July 2014, 1234 - 1238

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