| タイトル | Results of an Icing test on a NACA 0012 airfoil in the NASA Lewis Icing Research Tunnel |
| 本文（外部サイト） | http://hdl.handle.net/2060/19920005833 |
| 著者（英） | Shin, Jaiwon; Bond, Thomas H. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1992-01-01 |
| 言語 | eng |
| 内容記述 | Tests were conducted in the Icing Research Tunnel (IRT) at the NASA Lewis Research Center to document the current capability of the IRT, focused mainly on the repeatability of the ice shape over a range of icing conditions. Measurements of drag increase due to the ice accretion were also made to document the repeatability of drag. Surface temperatures of the model were obtained to show the effects of latent-heat release by the freezing droplets and heat transfer through the ice layer. The repeatability of the ice shape was very good at low temperatures, but only fair at near freezing temperatures. In general, drag data shows good repeatability. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 92N15051
E-6761
NAS 1.15:105374
NASA-TM-105374
AIAA PAPER 92-0647 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/129203 |
