| タイトル | Icing Test Results on an Advanced Two-Dimensional High-Lift Multi-Element Airfoil |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940029199 |
| 著者（英） | Chin, Vincent; Shin, Jaiwon; Wilcox, Peter; Sheldon, David |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1994-06-01 |
| 言語 | eng |
| 内容記述 | An experimental study has been conducted to investigate ice accretions on a high-lift, multi-element airfoil in the Icing Research Tunnel at the NASA Lewis Research Center. The airfoil is representative of an advanced transport wing design. The experimental work was conducted as part of a cooperative program between McDonnell Douglas Aerospace and the NASA Lewis Research Center to improve current understanding of ice accretion characteristics on the multi-element airfoil. The experimental effort also provided ice shapes for future aerodynamic tests at flight Reynolds numbers to ascertain high-lift performance effects. Ice shapes documented for a landing configuration over a variety of icing conditions are presented along with analyses. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 94N33705
NASA-TM-106620
E-8906
NAS 1.15:106620
AIAA PAPER 94-1869 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
