Sub-millimeter sized multi-component jet fuel surrogate droplet combustion: Physicochemical preferential vaporization effects-Reference-Cited by-同舟云学术

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Sub-millimeter sized multi-component jet fuel surrogate droplet combustion: Physicochemical preferential vaporization effects

Published:2021 Issue:2 Volume:38 Page:3313-3323
ISSN:1540-7489
Container-title:Proceedings of the Combustion Institute
language:en
Short-container-title:Proceedings of the Combustion Institute

Author:

Farouk Tanvir I.,Won Sang Hee,Dryer Frederick L.

Funder

Air Force Research Laboratory

National Aeronautics and Space Administration

Publisher

Elsevier BV

Subject

Physical and Theoretical Chemistry,Mechanical Engineering,General Chemical Engineering

Reference26 articles.

1. Chemical kinetic and combustion characteristics of transportation fuels

2. A combustion model for multi-component fuels using a physical surrogate group chemistry representation (PSGCR)

3. A jet fuel surrogate formulated by real fuel properties

4. The experimental evaluation of a methodology for surrogate fuel formulation to emulate gas phase combustion kinetic phenomena

5. Reconstruction of chemical structure of real fuel by surrogate formulation based upon combustion property targets

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2. The role of preferential vaporization in bi-component n-dodecane/iso-octane non-premixed spray cool flames;AIAA SCITECH 2024 Forum;2024-01-04

3. Preferential vaporization effects on the ignition of multi-component droplets;Proceedings of the Combustion Institute;2024

4. Analysis and flamelet modeling of preferential evaporation in SAF/Jet A spray flames;Proceedings of the Combustion Institute;2024

5. Experimental study of droplet vaporization for conventional and renewable transportation fuels: Effects of physical properties and chemical composition;Fuel;2024-01

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