Steam-Assisted Cracking of n-Dodecane in a Packed-Bed Reactor for Hypersonic Thermal Management
Author:
Affiliation:
1. University of Dayton, Dayton, Ohio 45469-0238
2. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433-7103
Funder
Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.T6035
Reference41 articles.
1. NuferB. “A Summary of NASA and USAF Hypergolic Propellant Related Spills and Fires,” AIAA Paper 2010-1994, April 2010. 10.2514/6.2010-1994
2. Heat Transfer Operability Limits for an Actively and Passively Cooled Hypersonic Vehicle
3. Efficient utilization of heat sink of hydrocarbon fuel for regeneratively cooled scramjet
4. Endothermic Pyrolysis of JP-10 with and without Zeolite Catalyst for Hypersonic Applications
5. Catalytic Cracking of Pure Hydrocarbons.
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2. Cerium Catalysts in Steam-Assisted Pyrolysis of n-Dodecane for Hypersonic Thermal Management;Journal of Thermophysics and Heat Transfer;2022-04
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