Abstract
This report investigates our present ability to predict the thermal performance of film cooling arrangements used to protect the hot components of gas turbines. The required information is usually obtained by model experiments carried out at near room temperature as opposed to the high temperature encountered in the gas turbines. Dimensional or similarity analysis is used to develope the functional relationships for film effectiveness and convective heat transfer and the use of mass transfer experiments with foreign gas injection and naphthalene sublimation based on the heat-mass transfer analogy is discussed. The law of superposition is used to describe the combined effects of film cooling, surface convection or radiation and frictional heating. An order of magnitude estimate indicates to what extent local temperature gradients are alleviated in the cooled walls by internal heat conduction.
Zusammenfassung
Die vorliegende Arbeit untersucht den gegenwärtigen Stand unserer Fähigkeit, die Wirksamkeit der Filmkühlung für Gasturbinen vorauszubestimmen. Die rechnerischen Unterlagen dazu werden meist durch Modellversuche bei mäßigen Temperaturen bestimmt, im Gegensatz zu den hohen Temperaturen in Gasturbinen. Ähnlichkeitsanalyse hilft dann zu ermitteln, inwieweit die durch Modellversuche erhaltenen Beziehungen auf den tatsächlichen Vorgang übertragbar sind. Die Analogie zwischen Wärme-und Stoffübergang eröffnet weitere Möglichkeiten für Modellversuche, und Superpositionsverfahren erlauben es, konvektiven Wärmeübergang und thermische Strahlung mit Filmkühlung zu kombinieren. Der Temperaturausgleich durch Wärmeleitung in der filmgekühlten Wand wird größenmäßig abgeschätzt.
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Abbreviations
- c p :
-
specific heat
- k :
-
thermal conductivity
- M :
-
blowing parameter
- p :
-
pressure
- Pr :
-
Prandtl number
- q :
-
heat flux per unit area
- R :
-
gas constant
- r :
-
recovery factor
- Re :
-
Reynolds number
- St :
-
Stanton number
- T :
-
Temperature
- t :
-
temperature difference
- u, v, w :
-
velocity components
- V :
-
Velocity
- x, y, z :
-
coordinates
- o :
-
upstream, at 300 K
- f :
-
film cooling
- l :
-
secondary fluid
- aw :
-
adiabatic wall surface
- H :
-
heat
- i :
-
isoenergetic
- M :
-
mass
- w :
-
wall surface
- α :
-
thermal diffusivity
- αβγ :
-
exponents
- ε :
-
turbulent diffusivity
- η :
-
film effectiveness
- ϱ :
-
density
- ν :
-
kinematic viscosity
- μ :
-
viscosity
References
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Dedicated to Prof. Dr.-Ing. U. Grigull's 80th birthday
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Eckert, E.R.G. Similarity analysis of model experiments for film cooling in gas turbines. Wärme- und Stoffübertragung 27, 217–223 (1992). https://doi.org/10.1007/BF01589919
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DOI: https://doi.org/10.1007/BF01589919