By Associate Professor Sudhir Laxman Gai

Journal articles

, 1996, 'Leading-edge bluntness effects in high enthalpy, hypersonic compression corner flow', AIAA Journal, 34, pp. 2284 - 2290, http://dx.doi.org/10.2514/3.13392

Petrusma MS; Gai SL, 1996, 'Bluff body wakes with free, fixed and discontinuous separation at low reynolds numbers and low aspect ratio', Experiments in Fluids, 20, pp. 189 - 198

Mallinson SG; Gai SL; Mudford NR, 1996, 'Leading edge bluntness effects in high enthalpy, Hypersonic flat plate flow', AIAA American Institute of Aeronautics and Astronautics Journal, pp. 2284 - 2290

Mallinson SG; Gai SL; Mudford NR, 1996, 'The boundary layer on a flat plate in hupervelocity flow', Aeronautical Journal, 100, pp. 135 - 141

Mallinson SG; Gai SL; Mudford NR, 1996, 'Upstream influence and peak heating in hypervelcotiy shock wave/Boundary layer interaction', Journal of Propulsion and Power, 12, pp. 984 - 990

Petrusma MS; Gai SL, 1994, 'Effect of geometry on the base pressure recovery of segmented blunt trailing edges', Aeronautical Journal, 98, pp. 267 - 274

Petrusma MS; Gai SL, 1994, 'Shedding frequency of segmented blunt trailing edges', Aeronautical Journal, 98, pp. 275 - 276

Gai SL; Mudford NR, 1992, 'Stagnation point heat flux in hypersonic high enthalpy flow', Shock Waves, 2, pp. 43 - 47, http://dx.doi.org/10.1007/BF01414420

Gai SL, 1992, 'Free piston shock tunnels: developments and capabilities', Progress in Aerospace Sciences, 29, pp. 1 - 41, http://dx.doi.org/10.1016/0376-0421(92)90002-Y

Gai SL; Joet WS, 1992, 'Laminar heat transfer to blunt cones in high-enthalpy hypervelocity flows', Journal of Thermophysics and Heat Transfer, 6, pp. 433 - 438, http://dx.doi.org/10.2514/3.379

Gai SL, 1992, 'Separated high enthalpy dissociated laminar hypersonic flow behind astep—Pressure measurements', AIAA Journal, 30, pp. 1915 - 1918, http://dx.doi.org/10.2514/3.11155

GAI SL; CAIN T; JOE WS, 1991, 'HEAT-TRANSFER MEASUREMENTS ON A BICONIC IN HYPERVELOCITY NITROGEN FLOW', AERONAUTICAL JOURNAL, 95, pp. 187 - 193, https://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:A1991FZ76600002&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=891bb5ab6ba270e68a29b250adbe88d1

Gai SL, 1989, 'A note on the vortex trail behind bluff bodies', Physics of Fluids A, 1, pp. 1288 - 1289, http://dx.doi.org/10.1063/1.857355

Gai SL; Reynolds NT; Ross C; Baird JP, 1989, 'Measurements of heat transfer in separated high-enthalpy dissociated laminar hypersonic flow behind a step', Journal of Fluid Mechanics, 199, pp. 541 - 561, http://dx.doi.org/10.1017/S0022112089000479

Gai SL; Lyons PRA, 1989, 'Shock standoff from blunt cones in high-enthalpy nonequilibrium nitrogen flow', AIAA Journal, 27, pp. 918 - 920, http://dx.doi.org/10.2514/3.10200

Gai SL, 1989, 'Shock wave asymmetry of sphere cones at angles of attack', Journal of Spacecraft and Rockets, 26, pp. 198 - 200, http://dx.doi.org/10.2514/3.26054

LYONS PRA; GAI SL, 1988, 'A METHOD FOR THE ACCURATE DETERMINATION OF THE THERMAL PRODUCT (RHO-CK)1/2 FOR THIN-FILM HEAT-TRANSFER OR SURFACE THERMOCOUPLE GAUGES', JOURNAL OF PHYSICS E-SCIENTIFIC INSTRUMENTS, 21, pp. 445 - 448, http://dx.doi.org/10.1088/0022-3735/21/5/005

Magi EC; Gai SL, 1988, 'Supersonic base pressure and lipshock', AIAA Journal, 26, pp. 370 - 372, http://dx.doi.org/10.2514/3.9900

Gai SL; Sharma SD, 1987, 'Pressure distributions behind a rearward facing segmented step', Experiments in Fluids, 5, pp. 154 - 158, http://dx.doi.org/10.1007/BF00298455

Sharma SD; Gai SL, 1987, 'Pressure distributions behind a rearward facing segmented step.', EXP. FLUIDS, 5

Gai SL; Sandeman RJ; Lyons P; Kilpin D, 1984, 'Shock shape over a sphere cone in hypersonic high enthalpy flow', AIAA Journal, 22, pp. 1007 - 1010, http://dx.doi.org/10.2514/3.48542

Gai SL; Sharma SD, 1984, 'Subsonic turbulent flow over a rearward facing segmented step', Physics of Fluids, 27, pp. 544 - 546, http://dx.doi.org/10.1063/1.864663

Lyons PRA; Kilpin D; Gai SL, 1984, 'A new high-speed electromechanical shutter', Journal of Physics E: Scientific Instruments, 17, pp. 108 - 110, http://dx.doi.org/10.1088/0022-3735/17/2/006

Gai SL; Sharma SD, 1981, 'EXPERIMENTS ON THE REDUCTION OF BASE DRAG OF A BLUNT TRAILING EDGE AEROFOIL IN SUBSONIC FLOW.', Aeronautical Journal, 85, pp. 206 - 210

Sarode RS; Gai SL; Ramesh CK, 1981, 'Flow around circular- and square-section models of finite height in a turbulent shear flow', Journal of Wind Engineering and Industrial Aerodynamics, 8, pp. 223 - 230, http://dx.doi.org/10.1016/0167-6105(81)90022-2

Sarode RS; Gai SL; Ramesh CK, 1981, 'Flow around circular- and square-section models of finite height in a turbulent shear flow.', J. WIND ENGNG. & IND. AERODYN., 8

Gai SL; Kapoor K, 1981, 'Jet Effects on near wake of an axisymmetric bluff body', Journal of Spacecraft and Rockets, 18, pp. 540 - 544, http://dx.doi.org/10.2514/3.28069

Gai SL; Patil SR, 1980, 'Subsonic axisymmetric base flow experiments with base modifications', Journal of Spacecraft and Rockets, 17, pp. 42 - 46, http://dx.doi.org/10.2514/3.28024

Gai SL, 1979, 'The centre-line velocity in the laminar near wake of a thin flat plate set parallel to a supersonic stream', Acta Mechanica, 31, pp. 281 - 283, http://dx.doi.org/10.1007/bf01176854

Gai SL, 1977, 'Incipient separation of leeward flow past a lifting plate in viscoushypersonic flow', AIAA Journal, 15, pp. 122 - 124, http://dx.doi.org/10.2514/3.7309

Gai SL, 1977, 'SHOCK-WAVE BOUNDARY-LAYER INTERACTION WITH SUCTION.', Z Flugwiss Weltraumforsch, 1, pp. 97 - 101

Gai SL, 1969, 'Effect of suction on the upstream influence in shockwave-boundary layer interactions', Zeitschrift für angewandte Mathematik und Physik ZAMP, 20, pp. 265 - 272, http://dx.doi.org/10.1007/BF01595566

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