Pressure Effects on Flowing Mildly-Cracked n-Decane
Author:
Affiliation:
1. University of Dayton, Dayton, Ohio 45469-0210
2. University of Dayton Research Institute, Dayton, Ohio 45469-0116
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.6863
Reference22 articles.
1. Hydrocarbon Fuel Cooling Technologies for Advanced Propulsion
2. Simulations of Flowing Mildly-Cracked Normal Alkanes Incorporating Proportional Product Distributions
3. Rapid Thermal Cracking of n-Hexadecane at Elevated Pressures
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