Conceptual Design of a Supercritical Oxyfuel Combustor Based on LOX/Methane Rocket Engine Technologies
Author:
Affiliation:
1. University of Texas, El Paso
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4636
Reference23 articles.
1. Separation and Capture of CO2from Large Stationary Sources and Sequestration in Geological Formations—Coalbeds and Deep Saline Aquifers
2. Assessment of oxy-fuel, pre- and post-combustion-based carbon capture for future IGCC plants
3. Two novel oxy-fuel power cycles integrated with natural gas reforming and CO2 capture
4. Qualitative and Quantitative Comparison of Two Promising Oxy-Fuel Power Cycles for CO2 Capture
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Innovative power generation systems using supercritical CO2 cycles;Clean Energy;2017-11-24
2. Preliminary Computational Analysis of Combustion in a Directly Heated Supercritical Oxy-Fuel Combustor;55th AIAA Aerospace Sciences Meeting;2017-01-05
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