| タイトル | Numerical solution for the temperature distribution in a cooled guide vane blade of a radial gas turbine |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770013162 |
| 著者（英） | Tabakoff, W.; Hosny, W. M. |
| 著者所属（英） | Cincinnati Univ. |
| 発行日 | 1977-01-01 |
| 言語 | eng |
| 内容記述 | A two dimensional finite difference numerical technique is presented to determine the temperature distribution of an internal cooled blade of radial turbine guide vanes. A simple convection cooling is assumed inside the guide vane blade. Such cooling has relatively small cooling effectiveness at the leading edge and at the trailing edge. Heat transfer augmentation in these critical areas may be achieved by using impingement jets and film cooling. A computer program is written in FORTRAN IV for IBM 370/165 computer. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 77N20106
NASA-CR-137943 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/182823 |
