Evaluation of the Physicochemical Authenticity of Aviation Kerosene Surrogate Mixtures. Part 1: Analysis of Volatility with the Advanced Distillation Curve

被引:53
作者
Bruno, Thomas J. [1 ]
Smith, Beverly L. [1 ]
机构
[1] Natl Inst Stand & Technol, Thermophys Properties Div, Boulder, CO 80305 USA
关键词
ROCKET PROPELLANTS RP-1; THERMAL-DECOMPOSITION KINETICS; THERMOPHYSICAL PROPERTIES; DIESEL FUEL; THERMODYNAMIC PROPERTIES; BIODIESEL FUEL; JET; MODEL; COMBUSTION; IMPROVEMENTS;
D O I
10.1021/ef100496j
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
Because of the complexities involved in measuring and modeling the performance and properties of finished fuels, the fuel science community must often use surrogate mixtures as substitutes, especially in the absence of consensus standard mixtures. While surrogate mixtures are often formulated on the basis of the ability of a particular mixture to reproduce a particular property, there is usually a desire to employ surrogate mixtures that are physicochemically authentic. This means that, provided that the primary purpose is satisfied, researchers are inclined to choose mixtures that have physical and chemical properties appropriate to the finished fuel. In this paper, we apply the advanced distillation curve method as a means to evaluate the physicochemical authenticity of surrogate mixtures. While the strategy outlined here can be used for any family of surrogates, we apply it to surrogate mixtures for Jet-A/JP-8. Mixtures were divided into two groups: (1) simple surrogate mixtures with up to three components and (2) complex surrogate mixtures with more than three components. We found that the modified Aachen surrogate (among the simple fluids) and the Schultz surrogate (among the complex fluids) had the best physicochemical authenticity.
引用
收藏
页码:4266 / 4276
页数:11
相关论文
共 82 条
  • [31] Advancements in gas turbine fuels from 1943 to 2005
    Edwards, Tim
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2007, 129 (01): : 13 - 20
  • [32] STATIC TESTS OF JET FUEL THERMAL AND OXIDATIVE STABILITY
    HENEGHAN, SP
    LOCKLEAR, SL
    GEIGER, DL
    ANDERSON, SD
    SCHULZ, WD
    [J]. JOURNAL OF PROPULSION AND POWER, 1993, 9 (01) : 5 - 9
  • [33] OXIDATION OF JET FUELS AND THE FORMATION OF DEPOSITS
    HENEGHAN, SP
    ZABARNICK, S
    [J]. FUEL, 1994, 73 (01) : 35 - 43
  • [34] Chemically authentic surrogate mixture model for the thermophysical properties of a coal-derived liquid fuel
    Huber, M. L.
    Lemmon, E. W.
    Diky, V.
    Smith, B. L.
    Bruno, T. J.
    [J]. ENERGY & FUELS, 2008, 22 (05) : 3249 - 3257
  • [35] Surrogate mixture model for the thermophysical properties of synthetic aviation fuel S-8: Explicit application of the advanced distillation curve
    Huber, M. L.
    Smith, B. L.
    Ott, L. S.
    Bruno, T. J.
    [J]. ENERGY & FUELS, 2008, 22 (02) : 1104 - 1114
  • [36] Surrogate Mixture Models for the Thermophysical Properties of Aviation Fuel Jet-A
    Huber, M. L.
    Lemmon, E. W.
    Bruno, T. J.
    [J]. ENERGY & FUELS, 2010, 24 (06) : 3565 - 3571
  • [37] Effect of RP-1 Compositional Variability on Thermophysical Properties
    Huber, M. L.
    Lemmon, E. W.
    Bruno, T. J.
    [J]. ENERGY & FUELS, 2009, 23 (11) : 5550 - 5555
  • [38] Preliminary Surrogate Mixture Models for the Thermophysical Properties of Rocket Propellants RP-1 and RP-2
    Huber, M. L.
    Lemmon, E. W.
    Ott, L. S.
    Bruno, T. J.
    [J]. ENERGY & FUELS, 2009, 23 (5-6) : 3083 - 3088
  • [39] Model for the Thermodynamic Properties of a Biodiesel Fuel
    Huber, Marcia L.
    Lemmon, Eric W.
    Kazakov, Andrei
    Ou, Lisa S.
    Bruno, Thomas J.
    [J]. ENERGY & FUELS, 2009, 23 (07) : 3790 - 3797
  • [40] Transport properties of n-dodecane
    Huber, ML
    Laesecke, A
    Perkins, R
    [J]. ENERGY & FUELS, 2004, 18 (04) : 968 - 975