Determination of the JP10 + OH → Product Reaction Rate with Measured Fuel Concentrations in Shock Tube Experiments
Author:
Affiliation:
1. Department of Mechanical Engineering, Stanford University, Stanford, California 94305, United States
Funder
Air Force Office of Scientific Research
Publisher
American Chemical Society (ACS)
Subject
Physical and Theoretical Chemistry
Link
https://pubs.acs.org/doi/pdf/10.1021/acs.jpca.0c00065
Reference16 articles.
1. Bruno, T. J.; Huber, M. L.; Laesecke, A.; Lemmon, E. W.; Perkins, R. A. Thermochemical and Thermophysical Properties of JP-10, NISTIR 6640, 2006.
2. Davidson, D. F.; Horning, D. C.; Oehlschlaeger, M. A.; Hanson, R. K. In The Decomposition Products of JP-10, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference; Salt Lake City, UT, July 8–11, 2001, AIAA 01-3707.
3. JP-10 combustion studied with shock tube experiments and modeled with automatic reaction mechanism generation
4. A theoretical study of JP-10 hydroperoxidation
5. Ignition Delay for Jet Propellant 10/Air and Jet Propellant 10/High-Energy Density Fuel/Air Mixtures
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