| タイトル | Analysis of Turbine Blade Relative Cooling Flow Factor Used in the Subroutine Coolit Based on Film Cooling Correlations |
| 本文（外部サイト） | http://hdl.handle.net/2060/20150011643 |
| 著者（英） | Schneider, Steven J. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2015-06-01 |
| 言語 | eng |
| 内容記述 | Heat transfer correlations of data on flat plates are used to explore the parameters in the Coolit program used for calculating the quantity of cooling air for controlling turbine blade temperature. Correlations for both convection and film cooling are explored for their relevance to predicting blade temperature as a function of a total cooling flow which is split between external film and internal convection flows. Similar trends to those in Coolit are predicted as a function of the percent of the total cooling flow that is in the film. The exceptions are that no film or 100 percent convection is predicted to not be able to control blade temperature, while leaving less than 25 percent of the cooling flow in the convection path results in nearing a limit on convection cooling as predicted by a thermal effectiveness parameter not presently used in Coolit. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | E-19070
GRC-E-DAA-TN20944
NASA/TM-2015-218738 |
| 権利 | No Copyright |
