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Sample size effect on the dynamic torsional behaviour of the 2A12 aluminium alloy
2017, 7(6): 317-324. doi: 10.1016/j.taml.2017.09.008
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Passive shock wave/boundary layer control of wing at transonic speeds
2017, 7(6): 325-330. doi: 10.1016/j.taml.2017.11.006
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Analysis of choked two-phase flows of gas and particle in a C-D nozzle
2017, 7(6): 331-338. doi: 10.1016/j.taml.2017.11.005
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Development of a high performance flexible porous burner (FPMB) with an adjustable cooling effect
2017, 7(6): 339-343. doi: 10.1016/j.taml.2017.11.007
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Effect of inclined ribs on heat transfer coefficient in stationary square channel
2017, 7(6): 344-350. doi: 10.1016/j.taml.2017.09.013
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2017, 7(6): 351-356. doi: 10.1016/j.taml.2017.11.009
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Aerodynamic improvement of a delta wing in combination with leading edge flaps
2017, 7(6): 357-361. doi: 10.1016/j.taml.2017.11.010
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2017, 7(6): 362-365. doi: 10.1016/j.taml.2017.11.008
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A study on characteristics of shock train inside a shock tube
2017, 7(6): 366-371. doi: 10.1016/j.taml.2017.09.005
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2017, 7(6): 372-378. doi: 10.1016/j.taml.2017.11.011
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Visualisation of air–water bubbly column flow using array Ultrasonic Velocity Profiler
2017, 7(6): 379-385. doi: 10.1016/j.taml.2017.09.014
2017 Vol.7 Issue 6
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