Laboratory for Hypersonic and Shockwave Research

Department of Aerospace Engineering

Indian Institute of Science, Bengaluru

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2000 - 2004

  1. Jagadeesh, G., Nataraja, K. N., & Udayakumar, M. (2004). Shock waves can enhance bacterial transformation with plasmid DNA. Current Science, 87(6), 734-735.

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  2. Saito, T., Menezes, V., Kuribayashi, T., Sun, M., Jagadeesh, G., & Takayama, K. (2003). Unsteady convective surface heat flux measurements on cylinder for CFD code validation. Shock Waves, 13(5), 327-337.

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  3. Joarder, R., & Jagadeesh, G. (2003). A new free floating accelerometer balance system for force measurements in shock tunnels. Shock Waves, 13(5), 409-412.

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  4. Ramjaun, D., Kato, I., Takayama, K., & Jagadeesh, G. (2003). Hypervelocity impacts on thin metallic and composite space debris bumper shields. AIAA journal, 41(8), 1564-1572.

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  5. Menezes, V., Saravanan, S., Jagadeesh, G., & J. Reddy, K. P. (2003). Experimental investigations of hypersonic flow over highly blunted cones with aerospikes. AIAA journal, 41(10), 1955-1966.

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  6. Sahoo, N., Mahapatra, D. R., Jagadeesh, G., Gopalakrishnan, S., & Reddy, K. P. J. (2003). An accelerometer balance system for measurement of aerodynamic force coefficients over blunt bodies in a hypersonic shock tunnel. Measurement Science and Technology, 14(3), 260.

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  7. Jagadeesh, G., Hashimoto, T., Naitou, K., Sun, M., & Takayama, K. (2003). Visualization of unsteady shock oscillations in the high-enthalpy flow field around double cones. Journal of visualization, 6(2), 195-203.

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  8. Sun, M., Yada, K., Jagadeesh, G., Onodera, O., Ogawa, T., & Takayama, K. (2003). A study of shock wave interaction with a rotating cylinder. Shock Waves, 12(6), 479-485.

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  9. Jagadeesh, G., & Takayama, K. (2002). Novel applications of micro-shock waves in biological sciences. Journal of Indian Institute of Science, 82, 1-10.

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  10. Jagadeesh, G., Nagashetty, K., Reddy, K. J., Sun, M., & Takayama, K. (2002). Studies on the effects of test gas on the flow field around large angle blunt cone flying at hypersonic Mach number. Transactions of the Japan Society for Aeronautical and Space Sciences, 45(149), 189-194.

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  11. Jagadeesh, G., Onodera, O., Ogawa, T., Takayama, K., & Jiang, Z. (2001). Micro-shock waves generated inside a fluid jet impinging on plane wall. AIAA journal, 39(3), 424-430.

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  12. Nagashetty, K., Saifuddin, S. K., Saravanan, S., Gurumurthy, K. S., Jagadeesh, G., & Reddy, K. P. J. (2000). Visualization of shock shapes around blunt bodies at hypersonic Mach number in a shock tunnel using electrical discharge technique. Current Science, 79(8), 1086-1089.

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  13. Jagadeesh, G., Reddy, N. M., Nagashetty, K., & J. Reddy, K. P. (2000). Forebody convective hypersonic heat transfer measurements over large-angle blunt cones. Journal of Spacecraft and Rockets, 37(1), 137-139.

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