Shock Tunnels and Hypersonic Research in IISc, Bangalore

Sriram, Rengarajan ; Jagadeesh, Gopalan (2015) Shock Tunnels and Hypersonic Research in IISc, Bangalore Experimental Methods of Shock Wave Research . pp. 347-378.

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Official URL: http://doi.org/10.1007/978-3-319-23745-9_11

Related URL: http://dx.doi.org/10.1007/978-3-319-23745-9_11

Abstract

The Laboratory for Hypersonic and Shock wave Research (LHSR), Department of Aerospace Engineering, Indian Institute of Science (IISc), Bangalore is a dedicated centre for the research, among other domains of fluid dynamics, on the shock dominated phenomena. More often than not, the focus of the research is on the flow phenomena at high enthalpies, which are addressed using the impulse facilities—shock tubes and tunnels. Ever since its inception as the High Enthalpy Aerodynamics Laboratory (HEAL) in the early 1970s the laboratory has pioneered in many domains of hypersonic and shock wave research in the country. The research from the laboratory has not only supported the hypersonic missions of national and global interests, but also has greatly contributed to the fundamental understanding of many aspects of high speed/shock dominated flows and their control. The present chapter describes the various shock tunnels in the laboratory and reviews some of the important research works carried out in these ground test facilities.

Item Type:Article
Source:Copyright of this article belongs to Springer Nature Switzerland AG.
Keywords:Mach Number; Heat Transfer Rate; Shock Tube; Drag Reduction; Separation Bubble
ID Code:127553
Deposited On:17 Oct 2022 04:36
Last Modified:17 Oct 2022 04:36

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