Experimental study of thermal-hydraulic characteristics of combustion chamber cooling channels with critical propulsion plant ribbing parameters
Authors: Aleksandrenkov V.P., Zubkov N.N., Yagodnikov D.A., Iryanov N.Ya., Sukhov A.V.
Published in issue: #10(58)/2016
DOI: 10.18698/2308-6033-2016-10-1545
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts
The article presents results of an experimental investigation studying thermal-hydraulic characteristics of combustion chamber cooling channels found in thermal propulsion plants characterised by a critically high ribbing level generated via deformational cutting technique. We show that these channels are operationally efficient when it comes to cooling high-temperature propulsion plant structures and provide reliable thermal shielding for said structures even in the case offilm boil occurring in the coolant.
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