1976
DOI: 10.1016/0010-2180(76)90026-2
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An investigation of the shock initiation of liquid nitromethane

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Cited by 66 publications
(44 citation statements)
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“…Arrows note where deviation from the unreacted universal liquid Hugoniot reference curve (shown in black) occurs, except for nitromethane, where no Hugoniot points have been reported above the reaction conditions, but reaction has been observed at the blue arrow at an induction time of ~200 ns. 13 These data appear to indicate that reactions require higher shock stress to occur within the time window of the shorter time measurements.…”
Section: Experimental Methodsmentioning
confidence: 88%
See 1 more Smart Citation
“…Arrows note where deviation from the unreacted universal liquid Hugoniot reference curve (shown in black) occurs, except for nitromethane, where no Hugoniot points have been reported above the reaction conditions, but reaction has been observed at the blue arrow at an induction time of ~200 ns. 13 These data appear to indicate that reactions require higher shock stress to occur within the time window of the shorter time measurements.…”
Section: Experimental Methodsmentioning
confidence: 88%
“…The shock is only supported for 300 ps, and all measurements are made during this time window. Figure 1 illustrates Hugoniot data for acrylonitrile, phenylacetylene, nitromethane, and carbon disulfide measured with plate impact data [8][9][10][11][12][13][14][15] recorded on nanosecond to microsecond time scales along with laser driven shock data measured on picosecond time scales. 4,5,16 The arrows mark the onset of deviation of the Hugoniot from the universal liquid Hugoniot along the particle velocity axis.…”
Section: Experimental Methodsmentioning
confidence: 99%
“…Many sets of the reaction rate parameters are available in the literature for liquid nitromethane. For example, (C, T A ) = (2.6 × 10 9 s −1 , 11,500 K) is suggested by Hardesty [14], (6.9 × 10 10 s −1 , 14,400 K) is used by Tarver and Urtiew [15] and (1.27 × 10 12 s −1 , 20,110 K) is used by Ripley et al [16]. In this work, we adopt the pre-exponential factor proposed by Hardesty [14] and adjust the activation temperature to T A = 11,350 K to match the experimentally calculated overtake time and the shape of the velocity versus distance graph of the shock-induced ignition experiment in Sheffield et al [17] (neat nitromethane, shocked at 9.1 GPa).…”
Section: Reaction Rates For Nitromethanementioning
confidence: 99%
“…For example, (C, T A ) = (2.6 × 10 9 s −1 , 11,500 K) is suggested by Hardesty [14], (6.9 × 10 10 s −1 , 14,400 K) is used by Tarver and Urtiew [15] and (1.27 × 10 12 s −1 , 20,110 K) is used by Ripley et al [16]. In this work, we adopt the pre-exponential factor proposed by Hardesty [14] and adjust the activation temperature to T A = 11,350 K to match the experimentally calculated overtake time and the shape of the velocity versus distance graph of the shock-induced ignition experiment in Sheffield et al [17] (neat nitromethane, shocked at 9.1 GPa). It should be noted that even though the single-step Arrhenius rate equation is a good starting point for investigating general trends associated with hot spot ignition and burn [18], care should be taken with regard to its pressure validity regime, as suggested (for pressures of 0.1-5GPa) by Shaw et al [19].…”
Section: Reaction Rates For Nitromethanementioning
confidence: 99%
“…It seemed worthwhile to extract Arrhenius parameters from the PETN wedge data in the usual way, 2s3s4 u~lng T2 ti-v '1~exp(TA/To) 1 TFTA whara v !s tha fraquancy factor, Tp is tha ttmparature rioe through the reaction zona, To 1s #hock tempera~ure, qnd TA Induction time tl waa extracted from tha wedge () 1 u-u '1 -t* , -r is activation temperature. data as where t* is time to detonation at the shock front, D is detonation velocity at the pracompraosad density, and U and u are sh~:k and particle v~locitiem r9apectlvely.…”
Section: A3stractmentioning
confidence: 99%