| タイトル | An analytical procedure and automated computer code used to design model nozzles which meet MSFC base pressure similarity parameter criteria |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810014654 |
| 著者（英） | Sulyma, P. R. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1980-05-01 |
| 言語 | eng |
| 内容記述 | Fundamental equations and similarity definition and application are described as well as the computational steps of a computer program developed to design model nozzles for wind tunnel tests conducted to define power-on aerodynamic characteristics of the space shuttle over a range of ascent trajectory conditions. The computer code capabilities, a user's guide for the model nozzle design program, and the output format are examined. A program listing is included. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 81N23187
NASA-CR-161775
LMSC-HREC-TR-D784111 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/169209 |
