Numerical Simulation of Pulse Detonation Engine with a Thermally Perfect Overall Reaction Model

2006 ◽  
Author(s):  
Kazuya Watanabe ◽  
Akiko Matsuo
Keyword(s):  
Numerical Simulation ◽  
Reaction Model ◽  
Pulse Detonation Engine ◽  
Pulse Detonation ◽  
Detonation Engine

scholarly journals Numerical simulation and performances evaluation of the pulse detonation engine

2018 ◽  
Vol 234 ◽  
pp. 01001 ◽  
Author(s):  
Vasile Prisacariu ◽  
Constantin Rotaru ◽  
Ionică Cîrciu ◽  
Mihai Niculescu
Keyword(s):  
Numerical Simulation ◽  
High Speed ◽  
Unmanned Vehicles ◽  
Working Fluid ◽  
Detonation Waves ◽  
Pulse Detonation Engine ◽  
Space Vehicles ◽  
Propulsion Systems ◽  
Pulse Detonation ◽  
Detonation Engine

A pulse detonation engine (PDE) is a type of propulsion system that uses detonation waves to combust the fuel and oxidizer mixture. The engine is pulsed because the mixture must be renewed in the combustor between each detonation wave. Theoretically, a PDE can operate from subsonic up to hypersonic flight speed. Pulsed detonation engines offer many advantages over conventional propulsion systems and are regarded as potential replacements for air breathing and rocket propulsion systems, for platforms ranging from subsonic unmanned vehicles, long range transports, high-speed vehicles, space launchers to space vehicles. The article highlights elements of the current state of the art, but also theoretical and numerical aspects of these types of unconventional engines. This paper presents a numerical simulation of a PDE at h=10000 m with methane as working fluid for stoichiometric combustion, in order to find out the detonation conditions.

scholarly journals Numerical simulation of the nozzle and ejector effect on the performance of a pulse detonation engine

2018 ◽  
Vol 22 (3) ◽  
pp. 1227-1237 ◽  
Author(s):  
Zhiwu Wang ◽  
Xing Liu ◽  
Yaqi Wang ◽  
Hongwei Li ◽  
Kun Zhang ◽  
...  
Keyword(s):  
Numerical Simulation ◽  
Pulse Detonation Engine ◽  
Pulse Detonation ◽  
Detonation Engine

scholarly journals Study on Influence of Diameter on Detonation Acoustic Characteristics of Pulse Detonation Engine

2020 ◽  
Vol 0 (0) ◽  
Author(s):  
Gui-yang Xu ◽  
Chun-guang Wang ◽  
Yan-fang Zhu ◽  
Hong-yan Li ◽  
Lun-kun Gong ◽  
...  
Keyword(s):  
Acoustic Characteristic ◽  
Pulse Detonation Engine ◽  
Acoustic Characteristics ◽  
Experiment System ◽  
Pulse Detonation ◽  
Impact Noise ◽  
Maximum Duration ◽  
Detonation Engine ◽  
Set Up ◽  
Different Diameters

AbstractThe experiment system of pulse detonation engine is set up to investigate on influence of diameter on detonation acoustic characteristic. The research of detonation acoustic characteristic of pulse detonation engine for four different diameters in different angles is carried out. Results from the test show that as the PDE diameter increasing, there are increases in amplitudes of impact noise in all angles, and the growth rate of amplitude of impact noise in the 90° direction is generally greater than that in the 0° direction. The smaller PDE diameter is, the distance of most obvious directivity at 0° turning to most obvious directivity at 30° is shorter. When the distance is shorter, such as 200 mm, the duration of detonation acoustic is increasing with the increase of PDE diameter, however, when the distance is longer, such as 3000 mm, it is just the opposite. The maximum duration of detonation acoustic is appeared in 3000 mm under 30 mm PDE diameter which reaches to 1.44 ms.

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