| タイトル | The method of complex characteristics for design of transonic blade sections |
| 本文（外部サイト） | http://hdl.handle.net/2060/19860021219 |
| 著者（英） | Bledsoe, M. R. |
| 著者所属（英） | New York Univ. |
| 発行日 | 1986-06-01 |
| 言語 | eng |
| 内容記述 | A variety of computational methods were developed to obtain shockless or near shockless flow past two-dimensional airfoils. The approach used was the method of complex characteristics, which determines smooth solutions to the transonic flow equations based on an input speed distribution. General results from fluid mechanics are presented. An account of the method of complex characteristics is given including a description of the particular spaces and coordinates, conformal transformations, and numerical procedures that are used. The operation of the computer program COMPRES is presented along with examples of blade sections designed with the code. A user manual is included with a glossary to provide additional information which may be helpful. The computer program in Fortran, including numerous comment cards is listed. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 86N30691
NASA-CR-176978
DOE/ER-03077/273
NAS 1.26:176978 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/153417 |
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