Evaluation of a Thermodynamic Ice Crystal Accretion Model using Experimental Data from NASA’s 2nd Fundamental Ice Crystal Icing TestA thermodynamic model describing ice crystal icing is evaluated using experimental data collected at NASA Propulsion Systems Laboratory. The model makes the distinction between ice accretions that are "freeze-dominated" and "melt-dominated". Freeze-dominated icing occurs when partially melted ice crystals impact a surface and freeze. This type of icing is characterized by strong adhesion. This contrasts with melt-dominated icing, where un-melted ice crystals adhere to a surface. This type of icing is characterized by weak adhesion. In this paper, the thermodynamic model is used to analyze the ice growth rates and facility conditions to explain possible phenomena such as mass loss as well as the melting and freezing fractions. Previous analyses assumed a collection efficiency of unity at the leading edge of the experimental model. LEWICE is used to determine a better estimate of the collection efficiency at the model leading edge as ice accretion grows in time. The result shows that the sticking efficiency could change in a greater percent with time than previously reported.
Document ID
20210017249
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Ru-Ching Chen (Glenn Research Center Cleveland, Ohio, United States)
Tadas Bartkus (Ohio Aerospace Institute Cleveland, Ohio, United States)
Jen-Ching Tsao (Ohio Aerospace Institute Cleveland, Ohio, United States)
Paul Von Hardenberg (Glenn Research Center Cleveland, Ohio, United States)
Thomas Ratvasky (Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
June 9, 2021
Subject Category
Aeronautics (General)
Meeting Information
Meeting: AIAA AVIATION Forum and Exposition
Location: Virtual
Country: US
Start Date: August 2, 2021
End Date: August 6, 2021
Sponsors: American Institute of Aeronautics and Astronautics