题名: |
Validation of NASA Thermal Ice Protection Computer Codes |
作者: |
Al-Khalil, Kamel M.; Horvath, Charles; Miller, Dean R.; Wright, William B. |
关键词: |
protection;computer;nasa;therm;code;erma;alid;simulation;prediction;naca0012 |
摘要: |
An experimental program was generated by the Icing Technology Branch at NASA Glenn Research Center to validate two ice protection simulation codes (1) LEWICE Thermal for transient electrothermal de-icing and anti-icing simulations, and (2) ANTICE for steady state hot gas and electrothermal anti-icing simulations. An electrothermal ice protection system was designed and constructed integral to a 36 inch chord NACA0012 airfoil. The model was fully instrumented with thermo-couples, RTD'S, and heat flux gages. Tests were conducted at several icing environmental conditions during a two week period at the NASA Glenn Icing Research Tunnel. Experimental results of running-wet and evaporative cases were compared to the ANTICE computer code predictions and are presented in this paper. |
报告类型: |
科技报告 |