Measurement of the Diffusion Coefficient of Water in RP-3 and RP-5 Jet Fuels Using Digital Holography Interferometry

Li, Chaoyue; Shao, Lei; Pan, Jun; Liu, Weihua

doi:10.1007/s10765-018-2373-4

Cited by 5 publications

(1 citation statement)

References 17 publications

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“…RP5 is a hydrocarbon fuel with a high density, viscosity, heat of combustion, and flash point that is widely used in carrier-based aircraft in China 8 . However, the dissolution characteristics of this fuel depend strongly on the material composition, temperature and pressure, and no universally accurate model is available to predict the gas solubility in RP5 from other known solubility data 9 , 10 .…”

Section: Introductionmentioning

confidence: 99%

Solubilities of CO2, O2 and N2 in rocket propellant 5 under low pressure

Feng

et al. 2022

Sci Rep

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The static method of isochoric saturation was used to measure the solubilities of CO2, O2 and N2 in rocket propellant 5 (RP5) at temperatures ranging from 253.15 to 323.15 K in 10 K intervals and pressures ranging from 0 to 120 kPa. The measurement accuracy of the constructed experimental setup was verified by measuring the solubility of CO2 in water. The relative expanded uncertainty (k = 2) in the solubility data was less than 4.0%. The solubilities of CO2, O2 and N2 in RP5 increased with pressure. As the temperature increased, the solubility decreased for CO2 solubility and increased for O2 and N2. Henry's constants for the three gases in RP5 decreased over the experimental temperature and pressure ranges in the order of N2 > O2 > CO2. The measured solubilities of CO2, O2 and N2 could be fitted with a modified Krichevsky–Kasarnovsky equation, and the maximum deviation between the measured and calculated data was less than 8.04%, 7.03% and 6.18%, respectively.

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Section: Introductionmentioning

confidence: 99%