4.7 Article

A physics based approach to modeling real-fuel combustion chemistry - IV. HyChem modeling of combustion kinetics of a bio-derived jet fuel and its blends with a conventional Jet A

期刊

COMBUSTION AND FLAME
卷 198, 期 -, 页码 477-489

出版社

ELSEVIER SCIENCE INC
DOI: 10.1016/j.combustflame.2018.07.012

关键词

Bio-derived jet fuel; Jet A; Hybrid Chemistry approach (HyChem); Fuel blends

资金

  1. Air Force Office of Scientific Research [FA9550-14-1-0235, FA9550-16-1-0195, FA9550-15-1-0409, FA9550-15-1-0496]
  2. National Aeronautics and Space Administration (NASA) [NNX15AV05A, NNX15AU96A]
  3. Federal Aviation Administration Office of Environment and Energy as a part of ASCENT Project 26 under FAA [13-CAJFE-SU-006, 13-C-AJFE-SU-016]
  4. Federal Aviation Administration Office of Environment and Energy as a part of ASCENT Project 35 under FAA [13-CAJFE-SU-006, 13-C-AJFE-SU-016]

向作者/读者索取更多资源

A Hybrid Chemistry (HyChem) approach has been recently developed for the modeling of real fuels; it incorporates a basic understanding about the combustion chemistry of multicomponent liquid fuels that overcomes some of the limitations of the conventional surrogate fuel approach. The present work extends this approach to modeling the combustion behaviors of a two-component bio-derived jet fuel (Gevo, designated as C1) and its blending with a conventional, petroleum-derived jet fuel (Jet A, designated as A2). The stringent tests and agreement between the HyChem models and experimental measurements for the combustion chemistry, including ignition delay and laminar flame speed, of C1 highlight the validity as well as potential wider applications of the HyChem concept in studying combustion chemistry of complex liquid hydrocarbon fuels. Another aspect of the present study aims at answering a central question of whether the HyChem models for neat fuels can be simply combined to model the combustion behaviors of fuel blends. The pyrolysis and oxidation of several blends of A2 and Cl were investigated. Flow reactor experiments were carried out at pressure of 1 atm, temperature of 1030 K, with equivalence ratios of 1.0 and 2.0. Shock tube measurements were performed for the blended fuel pyrolysis at 1 atm from 1025 to 1325 K. Ignition delay times were also measured using a shock-tube. Good agreement between measurements and model predictions was found showing that formation of the products as well as combustion properties of the blended fuels were predicted by a simple combination of the HyChem models for the two individual fuels, thus demonstrating that the HyChem models for two jet fuels of very different compositions are additive. (C) 2018 The Combustion Institute. Published by Elsevier Inc. All rights reserved.

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