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Reliable cooling of thermally high stressed components in the field of thrust chamber and turbine technology requires the use of more effective cooling techniques compared to the common recuperative cooling. Alternative cooling techniques basing on mass transfer through the wall such as transpiration cooling are available. For thermal design of transpiration cooled components a detailed knowledge with respect especially to the convective heat transfer behavior in the hot gas boundary layer on the porous wall is requested. This paper describes experimental investigations on this problem as well as the modeling of the measuring results by means of empirical correlations for engineering purposes.
Czasopismo
Rocznik
Tom
Strony
55--66
Opis fizyczny
Bibliogr. 3 poz.
Twórcy
autor
- Technische Universitat Dresden, Institute of Thermodynamics and Building Energy Systems, D-01062 Dresden, Germany, meinert@thermo.tu-dresden.de
Bibliografia
- [1] MEINERT, J.: Skin friction and heat transfer in a turbulent boundary layer with foreign gas transpiration, VDI Reports, Series 7, No. 402, 2000 (in German).
- [2] ROMANENKO, P.N., KHARCHENKO, V.N.: The effect of transverse mass flow on heat transfer and friction drag in a turbulent flow of compressible gas along an arbitrarily shaped surface, Int. J. of Heat and Mass Transfer 6 (1963), 727-738.
- [3] KAYS, W.M., CRAWFORD, M. E.: Convective heat and mass transfer, MacGraw Hill Book Company, 1980.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BGPK-0833-3284