Liquid Fuel Survey for Rotating Detonation Rocket Engines

2022 ◽  
Author(s):  
Alexis Harroun ◽  
Stephen D. Heister
Author(s):  
Blaine R. Bigler ◽  
John W. Bennewitz ◽  
Stephen A. Schumaker ◽  
Stephen A. Danczyk ◽  
William A. Hargus

Energies ◽  
2020 ◽  
Vol 13 (19) ◽  
pp. 5101
Author(s):  
Jan Kindracki ◽  
Krzysztof Wacko ◽  
Przemysław Woźniak ◽  
Stanisław Siatkowski ◽  
Łukasz Mężyk

Hydrogen is the most common molecule in the universe. It is an excellent fuel for thermal engines: piston, turbojet, rocket, and, going forward, in thermonuclear power plants. Hydrogen is currently used across a range of industrial applications including propulsion systems, e.g., cars and rockets. One obstacle to expanding hydrogen use, especially in the transportation sector, is its low density. This paper explores hydrogen as an addition to liquid fuel in the detonation chamber to generate thermal energy for potential use in transportation and generation of electrical energy. Experiments with liquid kerosene, hexane, and ethanol with the addition of gaseous hydrogen were conducted in a modern rotating detonation chamber. Detonation combustion delivers greater thermal efficiency and reduced NOx emission. Since detonation propagates about three orders of magnitude faster than deflagration, the injection, evaporation, and mixing with air must be almost instantaneous. Hydrogen addition helps initiate the detonation process and sustain continuous work of the chamber. The presented work proves that the addition of gaseous hydrogen to a liquid fuel–air mixture is well suited to the rotating detonation process, making combustion more effective and environmentally friendly.


Author(s):  
John W. Bennewitz ◽  
Jason R. Burr ◽  
Christopher F. Lietz

2005 ◽  
Vol 42 (3) ◽  
pp. 476-486 ◽  
Author(s):  
Andrea Bucchi ◽  
Claudio Bruno ◽  
Alessandro Congiunti

Author(s):  
Christopher Lietz ◽  
Nathan L. Mundis ◽  
Stephen A. Schumaker ◽  
Venke Sankaran

Shock Waves ◽  
2021 ◽  
Author(s):  
P. Wolański ◽  
W. Balicki ◽  
W. Perkowski ◽  
A. Bilar

AbstractResearch on the application of liquid fuels to continuously rotating detonation was conducted. A new method of mixture preparation was proposed. A special system of liquid fuel injection was designed and tested which is based on injecting into the detonation chamber a preheated liquid fuel partially mixed with hot air at conditions higher than the rich flammability limit. The specially selected conditions allow all liquid fuel to evaporate in the supply system but prevent it from ignition before entering the detonation chamber. Experiments were conducted for two different liquid fuels, extraction gasoline and Jet-A fuel. Research was carried out for different equivalence ratios, and in all tested conditions detonation was achieved. The new tested method of liquid fuel preparation and injection into a cylindrical detonation chamber opens a way of application of liquid fuels to engines which utilize continuously rotating detonation and thus prepares the way for practical application of detonative combustion to turbine engines and jet propulsion systems.


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