Development of the new criteria equations to compute the electrostatic field effect on intensification of heat transfer to the MS-20 motor aviation oil exposed to its forced convection
Published: 08.09.2025
Authors: Lvov M.V., Altunin V.A., Altunin K.V.
Published in issue: #9(165)/2025
DOI: 10.18698/2308-6033-2025-9-2477
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts
The paper presents results of an experimental study aimed at identifying the transverse electrostatic field effect on thermal processes in the MS-20 motor aviation oil exposed to its forced convection in the annular channel. The study includes various heat flux densities from a working heated metal tube, various pressures and oil pumping rates, various distances between the working coaxial needles and various supplied high electrostatic voltages. The study opens a possibility for the authors to create new experimental formulas for computing the heat transfer coefficient and to compare them with formulas by the other authors. Operability of the proposed new similarity criterion of the Al electric convection for the hydrocarbon fuels was tested in computing heat transfer to the MS-20 motor aviation oil. These formulas and methods application would facilitate a fast and high-quality computation, design and creation of new oil systems for the high-performance aircraft engines.
EDN RMWPGX
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