| タイトル | Characterization of Ice Roughness From Simulated Icing Encounters |
| 本文（外部サイト） | http://hdl.handle.net/2060/19970009633 |
| 著者（英） | Shin, Jaiwon; Anderson, David N. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1997-01-01 |
| 言語 | eng |
| 内容記述 | Detailed measurements of the size of roughness elements on ice accreted on models in the NASA Lewis Icing Research Tunnel (IRT) were made in a previous study. Only limited data from that study have been published, but included were the roughness element height, diameter and spacing. In the present study, the height and spacing data were found to correlate with the element diameter, and the diameter was found to be a function primarily of the non-dimensional parameters freezing fraction and accumulation parameter. The width of the smooth zone which forms at the leading edge of the model was found to decrease with increasing accumulation parameter. Although preliminary, the success of these correlations suggests that it may be possible to develop simple relationships between ice roughness and icing conditions for use in ice-accretion-prediction codes. These codes now require an ice-roughness estimate to determine convective heat transfer. Studies using a 7.6-cm-diameter cylinder and a 53.3-cm-chord NACA 0012 airfoil were also performed in which a 1/2-min icing spray at an initial set of conditions was followed by a 9-1/2-min spray at a second set of conditions. The resulting ice shape was compared with that from a full 10-min spray at the second set of conditions. The initial ice accumulation appeared to have no effect on the final ice shape. From this result, it would appear the accreting ice is affected very little by the initial roughness or shape features. |
| NASA分類 | Aerodynamics |
| レポートNO | 97N15029
NASA-TM-107400
NAS 1.15:107400
AIAA Paper 97-0052
E-10606 |
| 権利 | No Copyright |
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