By Associate Professor Sudhir Laxman Gai

Conference Papers

Vassilopoulos K; Gai SL; Petruma MS, 1995, 'Unsteady flow behind a blunt trailing edge aerofoil', in 33rd Aerospace Sciences Meeting and Exhibit

Gai SL; Milthorpe JF, 1993, 'Flow over a blunt stepped cone in hypersonic high enthalpy flow', in AIAA/DGLR 5th International Aerospace Planes and Hypersonics Technologies Conference, 1993, http://dx.doi.org/10.2514/6.1993-5152

TEH SL; GAI SL, 1992, 'INTERACTION OF AN INCIDENT CONICAL SHOCK WITH A BOUNDARY LAYER ON A FLAT PLATE', in Davis MR; Walker GJ (ed.), ELEVENTH AUSTRALASIAN FLUID MECHANICS CONFERENCE, VOLS 1 AND 2, UNIVERSITY TASMANIA, AUSTRALIA, UNIV TASMANIA, HOBART, pp. 43 - 46, presented at 11th Australasian Fluid Mechanics Conference, AUSTRALIA, UNIV TASMANIA, HOBART, 14 December 1992 - 18 December 1992, https://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:A1992BB94T00010&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=891bb5ab6ba270e68a29b250adbe88d1

MALLINSON SG; GAI SL; MUDFORD NR, 1992, 'LAMINAR FLOWS OF HIGH ENTHALPY AIR IN A COMPRESSION CORNER', in Davis MR; Walker GJ (ed.), ELEVENTH AUSTRALASIAN FLUID MECHANICS CONFERENCE, VOLS 1 AND 2, UNIVERSITY TASMANIA, AUSTRALIA, UNIV TASMANIA, HOBART, pp. 275 - 278, presented at 11th Australasian Fluid Mechanics Conference, AUSTRALIA, UNIV TASMANIA, HOBART, 14 December 1992 - 18 December 1992, https://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:A1992BB94T00066&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=891bb5ab6ba270e68a29b250adbe88d1

TEH SL; GAI SL, 1992, 'INTERACTION OF A CONICAL SHOCK-WAVE WITH A TURBULENT BOUNDARY-LAYER', in ICAS PROCEEDINGS 1992, VOLS 1 AND 2, AMER INST AERONAUTICS & ASTRONAUTICS, PEOPLES R CHINA, BEIJING, pp. 1647 - 1654, presented at 18th Congress of the International-Council-of-the-Aeronautical-Sciences, PEOPLES R CHINA, BEIJING, 20 September 1992 - 25 September 1992, https://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:A1992BA84L00210&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=891bb5ab6ba270e68a29b250adbe88d1

GAI S; MUDFORD N; HACKETT C, 1992, 'Heat flux and shock shape measurements on an Aeroassist Flight Experiment model in a high enthalpy free piston shock tunnel', in 28th Joint Propulsion Conference and Exhibit, American Institute of Aeronautics and Astronautics, presented at 28th Joint Propulsion Conference and Exhibit, http://dx.doi.org/10.2514/6.1992-3907

Gai SL; Mudford NR; Hackett C, 1992, 'Neat flux and shock shape measurements on an aeroassist flight experiment model in a high enthalpy free piston shock tunnel', in AIAA/ASME/SAE/ASEE 28th Joint Propulsion Conference and Exhibit, 1992

Gai SL; Lyons PRA; Baird JP; Sandeman RJ, 1986, 'SOME HEAT TRANSFER MEASUREMENTS OVER A SPHERE-CONE IN HIGH ENTHALPY NON-EQUILIBRIUM FLOW.', pp. 649 - 656

Baird JP; Lyons PRA; Gai SL, 1985, 'DENSITY AND VELOCITY PROFILES IN NON-EQUILIBRIUM LAMINAR BOUNDARY LAYERS IN AIR.', in AIAA Paper

Gai SL; Lyons PRA; Baird JP; Sandeman RJ, 1985, 'STAGNATION POINT HEAT TRANSFER IN HYPERSONIC HIGH ENTHALPY FLOW.', in AIAA Paper

Baird JP; Lyons PRA; Gai SL, 1984, 'EXPERIMENTAL STUDY OF NON-EQUILIBRIUM LAMINAR HYPERSONIC BOUNDARY LAYERS IN AIR.', in National Conference Publication - Institution of Engineers, Australia

Gai SL, 1984, 'EXPERIMENTAL STUDY OF THE FLOW PAST A FLAT PLATE AT INCIDENCE IN SUPERSONIC LOW DENSITY STREAM.', pp. 257 - 264

Gai SL; Lyons PRA; Baird JP; Sandeman RJ, 1984, 'HEAT TRANSFER MEASUREMENTS OVER A SPHERE-CONE IN HYPERSONIC HIGH ENTHALPY FLOW.', in National Conference Publication - Institution of Engineers, Australia

Conference Proceedings (Editor of)

Reim B; Panetta C; Samanes E; Gai SL; Milthorpe JF; Kleine HH, (eds.), 2007, 'Proc. 26th International Symposium on Shock Waves', Goettingen. Germany, presented at 26th International Symposium on Shock Waves, Goettingen. Germany, 15 July 2007 - 20 July 2007

Theses / Dissertations

Currao G, 2018, Experimental Study of Hypersonic Fluid Structure Interaction with Shock Impingement on a Cantilevered Plate

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