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Heat Transfer Research
Импакт фактор: 0.404 5-летний Импакт фактор: 0.8 SJR: 0.264 SNIP: 0.504 CiteScore™: 0.88

ISSN Печать: 1064-2285
ISSN Онлайн: 2162-6561

Выпуски:
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Heat Transfer Research

DOI: 10.1615/HeatTransRes.v33.i1-2.150
11 pages

Hydrodynamics and Heat Transfer of a Three-Dimensional Flow in a Film Cooling System

V. A. Kudryavtsev
Central Institute of Aircraft Engine Manufacturing, Moscow, Russia
A. I. Mayorova
P. I. Baranov Central Scientific Research Institute of Aircraft Engines, Moscow, Russian Federation
A. A. Sviridenkov
Central Institute of Aircraft Engine Manufacturing, Moscow, Russia

Краткое описание

We carry out experimental investigation of flow and heat transfer in a film-cooling mixing unit as well as numerical calculation on the basis of a 3d equations of turbulent flow. The fact that flow structure is independent of cooler mass flow rate, i.e., Reynolds number, and is determined only by geometry is established. The turbulence and heat transfer depend on both geometry and Reynolds number.


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