作者: N. Sharath , E. Arunan , K. P. J. Reddy , P. K. Barhai
DOI: 10.18520/CS/V108/I11/2083-2087
关键词: Kerosene 、 Hypersonic speed 、 Materials science 、 Ignition delay 、 Shock tube 、 Single pulse 、 Carene 、 Mechanics
摘要: Ignition delay experiments of 3-carene, a biofuel, have been carried out in single-pulse shock tube for three equivalence ratios, 0.5, 1 and 2. The temperature was varied from 1140 to 1606 K. In the above-mentioned conditions, ignition found vary 1.180 ms 144 μs. values 3-carene were be lower than those JP-10, kerosene-based fuel being considered hypersonic applications.