Published June 2006 | Version v1
Journal article

Numerical investigation of film cooling effectiveness on the curved surface

  • 1. Department of Aeronautical Engineering, Air Force Academy, Yesilyurt, 34806 Istanbul (Turkey) and Mechanical Engineering Faculty, Istanbul Technical University, Guemuessuyu, 34439 Istanbul (Turkey)
  • 2. Mechanical Engineering Faculty, Istanbul Technical University, Guemuessuyu, 34439 Istanbul (Turkey)

Description

This paper deals with a numerical investigation of the film cooling effectiveness on five different curved surfaces and a flat surface. The models consist of 11 rectangular cross-sectioned injection holes aligned in a single row. The blowing ratios are from 0.5 to 2.0, and the injection angle with respect to the horizontal plane is 30o. The hole geometry, the slope of the curved surface and the blowing ratio have important effects on the film cooling effectiveness. The results show that the film cooling effectiveness of a given curved surface, both along the mainstream and the spanwise direction, depends on the optimum selection of the parameters mentioned above

Additional details

Identifiers

DOI
10.1016/j.enconman.2005.07.010;
PII
S0196-8904(05)00180-9;

Publishing Information

Journal Title
Energy Conversion and Management
Journal Volume
47
Journal Issue
9-10
Journal Page Range
p. 1231-1246
ISSN
0196-8904
CODEN
ECMADL

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
37069371
Subject category
S71: CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS;
Descriptors DEI
FILM COOLING; GEOMETRY; MATHEMATICAL MODELS; NUMERICAL ANALYSIS; SURFACES
Descriptors DEC
COOLING; MATHEMATICS

Optional Information

Copyright
Copyright (c) 2005 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.