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Investigating and experimentally determining the characteristics…

Engineering Journal: Science and Innovation

# 12·2017 11

Investigating and experimentally determining

the characteristics of thermal-hydraulic processes

in the cooling channels of liquid rocket engine combustion

chambers featuring an extremely high degree of ribbing

© V.P. Aleksandrenkov, K.E. Kovalev, D.A. Yagodnikov

Bauman Moscow State Technical University, Moscow, 105005, Russia

Cooling system efficiency is one of the most important parameters affecting reliability of

liquid rocket engines (LRE). Using ribbed cooling channels in LRE combustion chambers

makes it possible to increase the area of the heat-releasing surface, increasing the cool-

ing system efficiency. Employing additive manufacturing and the deformational cutting

technique for producing LRE combustion chambers looks promising, since it may lead to

maximising the heat-releasing surface area. The article considers a test installation de-

veloped to determine characteristics of thermal-hydraulic processes taking place in cool-

ing channels of LRE combustion chambers featuring an extremely high degree of ribbing,

manufactured with the help of additive technology and deformational cutting. We present

the design of prototype working segments of a combustion chamber featuring an extreme-

ly ribbed cooling channel. We developed a system for recording thermal-hydraulic char-

acteristics using high-accuracy digital transducers. We developed techniques for experi-

mentally investigating the characteristics of thermal-hydraulic processes in cooling

channels, computing heat transfer coefficients and friction loss in order to validate the

possibility of using cooling channels featuring an extremely high degree of ribbing in

LRE combustion chambers.

Keywords:

thermal-hydraulic characteristics, cooling channel, combustion chamber rib-

bing, additive manufacturing, deformational cutting

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