AIAA Propulsion and Energy 2019 Forum 2019
DOI: 10.2514/6.2019-3952
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Detonation Limits and Velocity Deficits of CH4, C2H4, C2H6 and C3H8 with N2O in a Small Diameter Tube

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Cited by 2 publications
(2 citation statements)
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“…Detonation experiments on CH 4 –, C 2 H 4 –, C 2 H 6 –, and C 3 H 8 –N 2 O mixtures with equivalence ratios from 0.4 to 2.0 were conducted by Hageman et al, using a tube and a Schelkin spirale for detonation initiation. The authors measured detonation limits and velocities, which were found to be consistently 2%–8% lower than the calculated Chapman–Jouguet velocities.…”
Section: Forced Ignitions Of N2o–h2 and N2o–hydrocarbon Mixturesmentioning
confidence: 99%
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“…Detonation experiments on CH 4 –, C 2 H 4 –, C 2 H 6 –, and C 3 H 8 –N 2 O mixtures with equivalence ratios from 0.4 to 2.0 were conducted by Hageman et al, using a tube and a Schelkin spirale for detonation initiation. The authors measured detonation limits and velocities, which were found to be consistently 2%–8% lower than the calculated Chapman–Jouguet velocities.…”
Section: Forced Ignitions Of N2o–h2 and N2o–hydrocarbon Mixturesmentioning
confidence: 99%
“…189 The detonation velocity was correlated with acetylene concentration in lean and stoichiometric C 2 H 2 −N 2 O mixtures. Zhang et al 190 191 using a tube and a Schelkin spirale for detonation initiation. The authors measured detonation limits and velocities, which were found to be consistently 2%−8% lower than the calculated Chapman−Jouguet velocities.…”
Section: Iii32 Laminar Burningmentioning
confidence: 99%