scholarly journals A preliminary heat transfer analysis of pulse detonation engines

2018 ◽  
Vol 29 ◽  
pp. 279-288 ◽  
Author(s):  
Berke Olcucuoglu ◽  
Bayindir H. Saracoglu
Keyword(s):  
Heat Transfer ◽  
Heat Transfer Analysis ◽  
Pulse Detonation Engines ◽  
Pulse Detonation

Experimental investigations of momentum and heat transfer in pulse detonation engines

2002 ◽  
Vol 29 (2) ◽  
pp. 2847-2854 ◽  
Author(s):  
Jiro Kasahara ◽  
Kouki Takazawa ◽  
Takakage Arai ◽  
Yu Tanahashi ◽  
Shingo Chiba ◽  
...  
Keyword(s):  
Heat Transfer ◽  
Experimental Investigations ◽  
Pulse Detonation Engines ◽  
Pulse Detonation ◽  
Momentum And Heat Transfer

A Numerical Simulation of Heat Pipe Application to the Cooling of Pulse Detonation Engines

2003 ◽  
Author(s):  
V. Dakshina Murty
Keyword(s):  
Heat Transfer ◽  
Heat Pipe ◽  
Stokes Equations ◽  
Navier Stokes ◽  
Brinkman Model ◽  
Navier Stokes Equations ◽  
Pulse Detonation Engines ◽  
Pulse Detonation ◽  
Flow And Heat Transfer ◽  
Detonation Tube

A numerical method based on the finite elements is applied to the cooling of pulse detonation tube using heat pipe technology. Towards this end, the fluid flow and heat transfer in the wick are modeled as flow in a porous medium. The flow is described using the so called Darcy Brinkman model which has close resemblance to the Navier-Stokes equations. It is found that for Darcy numbers less than 0.0001 the results are indistinguishable from regular Darcy flows. The shape of the heat pipe is that of a fin with the proportion of the length of the evaporator section being varied. In this study two values of this ratio have been used, namely 1 and 0.5.

FLOW FIELD AND HEAT TRANSFER ANALYSIS IN AMON/MMH BIPROPELLANT ROCKET ENGINE

2017 ◽  
Vol 16 (3) ◽  
pp. 263-280 ◽  
Author(s):  
Yu Daimon ◽  
Hideyo Negishi ◽  
Hiroumi Tani ◽  
Yoshiki Matsuura ◽  
Shigeyasu Iihara ◽  
...  
Keyword(s):  
Heat Transfer ◽  
Flow Field ◽  
Rocket Engine ◽  
Heat Transfer Analysis
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