Waste heat from a pulse detonation engine (PDE) was extracted via concentric, counter flow heat exchangers to produce supercritical pyrolytic conditions for JP-7 and JP-8 fuels. A sampling system and method was utilized to collect samples of reacted fuel to be extracted during steady state operation. Samples were collected over a range of heat exchanger exit temperatures from 820 K (1016° F) to 940 K (1232 degrees F) and for two sets of heat exchangers, one set coated with zeolite catalyst and one set left uncoated. Variation in fuel mass flow rate required the calculation of heat addition as an alternate to heat exchanger exit temperature as the independent variable when comparing fuel decomposition and engine performance. Offline chemical...
Understanding the impact of fuel characteristic differences on combustion behaviors such as cold sta...
Thesis (Ph.D.)--University of Washington, 2014Synthetic jet fuels are studied to help understand the...
A pulse detonation engine (PDE) is possible to be a next-generation high-performance propulsion syst...
Waste heat from a pulse detonation engine (PDE) was extracted via concentric, counter flow heat exch...
Waste heat from a pulse detonation engine (PDE) was extracted via zeolite catalyst coated concentric...
Every generation of advanced military aircraft fly higher and faster than previous generations. With...
Research has shown that performance of liquid hydrocarbon fueled pulse detonation engines is limited...
Pulse detonation engines (PDE) rely on rapid ignition and formation of detonation waves. Because hyd...
As modern hypersonic aircraft designs evolve, increasing heat sink capabilities are required. One p...
Pulse Detonation Engines (PDE) operating on liquid hydrocarbon fuels are limited to operating freque...
AbstractThe regenerative cooling technology is a promising approach for effective thermal protection...
Traditional fuel system designs do not provide the combination of sucient cooling and low system wei...
To more effectively utilize jet fuel as a thermal management fluid on board an aircraft, it is neces...
Practical air-breathing pulse detonation engines (PDE) will be based on storable liquid hydrocarbon ...
Current research by the US Air Force and Navy is concentrating on obtaining detonations in a pulse d...
Understanding the impact of fuel characteristic differences on combustion behaviors such as cold sta...
Thesis (Ph.D.)--University of Washington, 2014Synthetic jet fuels are studied to help understand the...
A pulse detonation engine (PDE) is possible to be a next-generation high-performance propulsion syst...
Waste heat from a pulse detonation engine (PDE) was extracted via concentric, counter flow heat exch...
Waste heat from a pulse detonation engine (PDE) was extracted via zeolite catalyst coated concentric...
Every generation of advanced military aircraft fly higher and faster than previous generations. With...
Research has shown that performance of liquid hydrocarbon fueled pulse detonation engines is limited...
Pulse detonation engines (PDE) rely on rapid ignition and formation of detonation waves. Because hyd...
As modern hypersonic aircraft designs evolve, increasing heat sink capabilities are required. One p...
Pulse Detonation Engines (PDE) operating on liquid hydrocarbon fuels are limited to operating freque...
AbstractThe regenerative cooling technology is a promising approach for effective thermal protection...
Traditional fuel system designs do not provide the combination of sucient cooling and low system wei...
To more effectively utilize jet fuel as a thermal management fluid on board an aircraft, it is neces...
Practical air-breathing pulse detonation engines (PDE) will be based on storable liquid hydrocarbon ...
Current research by the US Air Force and Navy is concentrating on obtaining detonations in a pulse d...
Understanding the impact of fuel characteristic differences on combustion behaviors such as cold sta...
Thesis (Ph.D.)--University of Washington, 2014Synthetic jet fuels are studied to help understand the...
A pulse detonation engine (PDE) is possible to be a next-generation high-performance propulsion syst...