Abstract
High-energy-density liquid fuels have been synthesized and used because they can provide more volumetric propulsion energy than conventional petroleum-derived aviation turbine fuels, thereby potentially increasing the maximum flight range and airspeed of aircraft. However, cyclic hydrocarbons in high-energy-density fuels have lower hydrogen contents than those in conventional normal paraffin fuels, resulting in a long ignition delay and a low combustion completion level, especially when the aerocraft is operating at low air pressure, high altitude, and low oxygen/fuel ratio conditions for hypersonic flights. An effective technology to improve the fuel ignition property is to use a catalyst to accelerate the fuel's combustion reaction at a relative low temperature. In this chapter, we summarize typical techniques to analyze the combustion process, combustion characters of fuels, and the methods to enhance ignition and combustion.
Original language | English |
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Title of host publication | High-Energy-Density Fuels for Advanced Propulsion |
Subtitle of host publication | Design and Synthesis |
Publisher | wiley |
Pages | 437-473 |
Number of pages | 37 |
ISBN (Electronic) | 9783527823789 |
ISBN (Print) | 9783527346691 |
DOIs | |
Publication status | Published - 5 Jun 2020 |
Externally published | Yes |
Keywords
- Catalyst
- Combustion
- High-energy-density fuels
- Ignition