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Conference Paper

Saravanan, S and Nagashetty, K and Jagadeesh, G and Reddy, KPJ (2009) Experimental investigation of heat transfer reduction using forward facing cavity for missile shaped bodies flying at hypersonic speed. In: 26th International Symposium on Shock Waves, JUL 15-20, 2007, Gottingen, Germany, pp. 613-617.

Reddeppa, P and Nagashetty, K and Jagadeesh, G (2009) Investigations of separated flow over backward facing steps in IISc hypersonic shock tunnel. In: 26th International Symposium on Shock Waves, JUL 15-20, 2007, Gottingen, Germany, pp. 631-636.

Hemanth, K and Jagadeesh, G and Saravanan, S and Nagashetty, K and Reddy, KPJ (2009) Shock tunnel testing of a Mach 6 hypersonic waverider. In: 26th International Symposium on Shock Waves, JUL 15-20, 2007, Gottingen, Germany, pp. 701-706.

Reddeppa, P and Nagashetty, K and Saravanan, S and Nayak, MM and Jagadeesh, G (2008) Direct skin friction measurement in IISc hypersonic shock tunnel. In: Proceedings of 24th Annual Inhouse Symposium on Space Science and Technology , January 2008, Bangalore.

Jagadeesh, G and Sriram, S and Saravanan, S and Nagashetty, K and Reddy, KPJ (2008) Experimental investigations on the effect of a thermal bump in the hypersonic flow around a flat plate. In: 47th AIAA Aerospace Meeting and Exhibit, Orlando USA, Orlando.

Saravanan, S and Reddy, KPJ and Nagashetty, K and Jagadeesh, G (2006) Free-floating accelerometer force balance for shock tunnel testing. In: 5th International Symposium on Strain gauge balances , May 2006, ONERA, France.

Jagadeesh, G and Sun, M and Nagashetty, K and Reddy, KRJ (2001) Experimental investigations of test gas effects on the hypersonic flow field around large angle blunt cone in shock tunnel. In: 39th Aerospace Sciences Meeting and Exhibit, 08 - 11 January 2001, Reno,NV,U.S.A..

Jagadeesh, G and Nagashetty, K and Rao, BRS and Reddy, KPJ (2001) Gas temperature layer visualization in hypersonic shock tunnel using electric discharge. In: 24th International Congress on High-Speed Photography and Photonics, 24-29 Sept. 2000, Sendai, Japan, pp. 864-871.

Nagashetty, K and Saifuddin, KS and Saravanan, S and Gurumurthy, KS and Reddy, KPJ (2001) Shock stand-off distance visualization in hypersonic shock tunnel using electrical discharge technique. In: 24th International Congress on High-Speed Photography and Photonics, 24-29 Sept. 2000, Sendai, Japan, pp. 674-681.

Journal Article

Reddeppa, P and Nagashetty, K and Saravanan, S and Jagadeesh, G and Gai, SL (2011) Measurement of Heat Transfer Rate on Backward-Facing Steps at Hypersonic Mach Number. In: Journal of Thermophysics and Heat Transfer, 25 (3). pp. 321-328.

Saravanan, S and Nagashetty, K and Hegde, GM and Jagadeesh, G and Reddy, KPJ (2011) Schlieren visualization of shock wave phenomena over a missile-shaped body at hypersonic Mach numbers. In: Proceedings of the Institution of Mechanical Engineers - Part G: Journal of Aerospace Engineering, 225 (G1). pp. 26-34.

Nagashetty, K and Reddy, KPJ and Jagadeesh, G and Rao, BRS and Satheesh, K and Saravanan, S (2004) Force measurements on hypersonic waveriders in the IISc hypersonic shock tunnel HST2. In: Shock Waves, 1-2 (3). pp. 341-346.

Nagashetty, K and Saifuddin, Syed K and Saravanan, S and Gurumurthy, KS and Jagadeesh, G and Reddy, KPJ (2000) Visualization of shock shapes around blunt bodies at hypersonic Mach number in a shock tunnel using electrical discharge technique. In: Current Science, 79 (8). pp. 1086-1089.

Jagadeesh, G and Reddy, NM and Nagashetty, K and Reddy, KPJ (2000) Forebody convective hypersonic heat transfer measurements over large-angle blunt cones. In: Journal of Spacecraft and Rockets, 37 (01). pp. 137-139.

Reddy, NM and Nagashetty, K and Jagadeesh, G and Reddy, KPJ (1996) Review of hypersonic research investigations in IISc shock tunnel (HST1). In: Sadhana : Academy Proceedings in Engineering Sciences, 21 (part 6). pp. 741-773.

Jagadeesh, G and Rao, Srinivasa BR and Nagashetty, K and Reddy, NM and Reddy, KPJ (1996) A new technique for visualization of shock shapes in hypersonic shock tunnel. In: Current Science, 71 (2). pp. 128-130.