AbstractA novel differential pressurization pulse jet engine is suggested in this paper. Working process of the engine is firstly introduced, then several realistic assumptions are made, physical model and mathematical model of the engine's extrusion and filling process are built. Using Propane as fuel, the mathematical model can be solved by setting some parameters. Working characteristics of the engine in each stage are analysed, and performance parameters of the engine is estimated, such as pressure, thrust, and specific impulse. Through suitably changing several structure parameters, analysing the performance parameters, the impacts of structural parameters on the engine performance are discussed. Finally, compared with conventional pul...
A pulse detonation engine (PDE) is a type of propulsion system that uses detonation waves to combust...
Simple design and efficiency make pulsejet engines attractive for aeronautical short-term operation ...
A pulse detonation engine has high thermal efficiency for utilizing detonation and is planned to var...
AbstractA novel differential pressurization pulse jet engine is suggested in this paper. Working pro...
The objective of this project work is to understand the thermodynamic characteristics of conventiona...
This project develops a computational study of an engine called pulsejet. Pulse jets were the first ...
The performance of an ideal, air breathing Pulse Detonation Engine is described in a manner that is ...
AbstractExperimental research of a valve pulse-jet engine can provide theoretical support and experi...
The Pulsejet is an unsteady propulsive device, with reed valves being the only moving parts in the e...
In order to obtain the dynamic operating characteristics of a pulse detonation turbine engine (PDTE)...
This research introduces the reader to a brief analysis of various types of aircraft engines, with p...
Quasi-steady state and transient state performance analyses of a pulse detonation turbine engine (PD...
An analytical model for predicting the performance of a single-tube air-breathing pulse detonation e...
Ejectors (jet pumps, jet devices) are widely used in various branches of engineering. They are used...
An experimental investigation on the developmental studies of the pulsejet was undertaken at NAL as ...
A pulse detonation engine (PDE) is a type of propulsion system that uses detonation waves to combust...
Simple design and efficiency make pulsejet engines attractive for aeronautical short-term operation ...
A pulse detonation engine has high thermal efficiency for utilizing detonation and is planned to var...
AbstractA novel differential pressurization pulse jet engine is suggested in this paper. Working pro...
The objective of this project work is to understand the thermodynamic characteristics of conventiona...
This project develops a computational study of an engine called pulsejet. Pulse jets were the first ...
The performance of an ideal, air breathing Pulse Detonation Engine is described in a manner that is ...
AbstractExperimental research of a valve pulse-jet engine can provide theoretical support and experi...
The Pulsejet is an unsteady propulsive device, with reed valves being the only moving parts in the e...
In order to obtain the dynamic operating characteristics of a pulse detonation turbine engine (PDTE)...
This research introduces the reader to a brief analysis of various types of aircraft engines, with p...
Quasi-steady state and transient state performance analyses of a pulse detonation turbine engine (PD...
An analytical model for predicting the performance of a single-tube air-breathing pulse detonation e...
Ejectors (jet pumps, jet devices) are widely used in various branches of engineering. They are used...
An experimental investigation on the developmental studies of the pulsejet was undertaken at NAL as ...
A pulse detonation engine (PDE) is a type of propulsion system that uses detonation waves to combust...
Simple design and efficiency make pulsejet engines attractive for aeronautical short-term operation ...
A pulse detonation engine has high thermal efficiency for utilizing detonation and is planned to var...