Shock Tunnels and Hypersonic Research in IISc, Bangalore
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Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-23745-9_11
Reference37 articles.
1. Reddy, N.M.: Development of a hypersonic shock tunnel. Proc. Indian Acad. Sci. Sect. C: Eng. Sci. 1(1), 73–92 (1978)
2. Reddy, N.M., Nagashetty, K., Jagadeesh, G., Reddy, K.P.J.: Review of hypersonic research investigations in IISc shock tunnel (HST-1). Sadhana 21(6), 741–773 (1996)
3. Joshi, M.V., Reddy, N.M.: Aerodynamic force measurements over missile configurations in IISc shock tunnel at M∞ = 5.5. Exp. Fluids 4(6), 338–340 (1986)
4. Raju, C., Reddy, N.M.: Aerodynamic force measurements over missile configurations in IISc shock tunnel at M∞ = 3.85 and 9.15. Exp. Fluids 10(2–3), 175–177 (1990)
5. Jagadeesh, G., Rao, B.K.S., Nagashetty, K., Reddy, N.M., Reddy, K.P.J.: Electrical discharge technique for three-dimensional flow field visualization in hypersonic shock tunnel. J Flow Vis. Image Process. 1(1), 51–57 (1997)
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