| タイトル | Blading models for TURBAN and CSPAN turbomachine design codes |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940006731 |
| 著者（英） | Glassman, Arthur J. |
| 著者所属（英） | Toledo Univ. |
| 発行日 | 1993-07-01 |
| 言語 | eng |
| 内容記述 | Blading models added to TURBAN, an axial turbine meanline design code, and CSPAN, an axial compressor spanline design code, are presented. Calculations of blade chord length, blade axial length, and number of blades for each blade row are now provided by each code. In order to accomplish this, computational models for axial solidity and stagger angle were added to TURBAN. For a compressor, where solidity and chord were already available from input, the modeling additions to CSPAN were for stagger angle and for the blade angles to include incidence and deviation. All added computations utilized models already available in the literature. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 94N11203
NASA-CR-191164
E-7997
NAS 1.26:191164 |
| 権利 | No Copyright |
|
