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Information Journal Paper

Title

Hypersonic ow over hemispherical blunt body with spikes

Pages

  358-366

Abstract

 Use of spike on a hemispherical body changes the ow eld and hence, the aerodynamic drag. Computational studies have been carried out to obtain the ow eld around a hemispherical body with spikes at a hypersonic Mach number of 6. The e ect of shape of spike tip and length has been studied. Laminar computations have been made adopting structured grid using commercial software FLUENT. It is observed that use of a sharp spike itself reduces the drag signi cantly. However, the use of a Hemispherical head spike further reduces the drag. Contribution of di erent components towards drag indicates that the increase in length of a spike does not change the spike contribution. However, the ow eld on main body is altered, which leads to reduction in drag with change in length. The estimated maximum drag is found to be highest among all reported drag values with any spike shape and length in the literature.

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  • Cite

    APA: Copy

    DAS, S., KUMAR, P., & PRASAD, J.K.. (2019). Hypersonic ow over hemispherical blunt body with spikes. SCIENTIA IRANICA, 26(1 (Transactions B: Mechanical Engineering)), 358-366. SID. https://sid.ir/paper/290685/en

    Vancouver: Copy

    DAS S., KUMAR P., PRASAD J.K.. Hypersonic ow over hemispherical blunt body with spikes. SCIENTIA IRANICA[Internet]. 2019;26(1 (Transactions B: Mechanical Engineering)):358-366. Available from: https://sid.ir/paper/290685/en

    IEEE: Copy

    S. DAS, P. KUMAR, and J.K. PRASAD, “Hypersonic ow over hemispherical blunt body with spikes,” SCIENTIA IRANICA, vol. 26, no. 1 (Transactions B: Mechanical Engineering), pp. 358–366, 2019, [Online]. Available: https://sid.ir/paper/290685/en

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