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A Department of Aerospace Engineering graduate student observes ice accretion in the department’s icing research tunnel, which was used for the research paper experiments.
11.22.2022

Hui Hu icing research study receives AIAA best paper honors

By John Burnett-Larkins, Iowa State University College of Engineering

A paper published by Department of Aerospace Engineering Martin C. Jischke Professor Hui Hu and three of his students has been selected to receive national recognition by the American Institute of Aeronautics and  Astronautics’ (AIAA) Gas Turbine Engines Technical Committee.

“An Experimental Study on the Dynamic Ice Accretion Process over the Surfaces of the Rotating Fan Blades of an Aero-Engine Model” (AIAA 2022-2435) has been chosen to receive the 2022 AIAA Gas Turbine Engine Best Paper Award. The paper is co-authored by three of Dr. Hu’s former Ph.D. students, including Dr. Dr. Linchuan Tian (currently a post-doctoral researcher at Shanghai Jiao Tong University); Dr. Linkai Li (currently an assistant professor at Nanjing University of Aeronautics and Astronautics); and Dr. Haiyang Hu (currently a post-doctoral researcher at Iowa State University with Prof. Hui Hu).

Hui Hu has been invited to attend the Technical Committee meeting during the AIAA SciTech 2023 Forum next January, where the paper will be officially honored.

The paper involves an experimental campaign conducted to study dynamic ice accretion on rotating aeroengine fan blades and evaluation of the icing-induced performance degradation to the fan rotor for the development of more effective and robust anti-/deicing strategies to ensure safer and more efficient operation of aeroengines in cold weather.

The experiments were performed in the Department of Aerospace Engineering’s icing research tunnel. It found, among other things, that aerodynamic performance of a fan rotor degraded substantially due to much rougher surfaces of iced fan blades. Needle-like icicles were found to grow rapidly out from the surfaces of the engine’s rotating spinner and fan blades under glaze icing conditions, due to the combined effects of the aerodynamic forces and the centrifugal forces associated with the rotation motion. This caused tremendous detrimental effects on the aerodynamic performance of the fan rotor.

Read the full abstract.

The paper will receive a “Best Paper” designation in the online library Aerospace Research Central (ARC) arc.aiaa.org that will last in perpetuity; and will be listed in the November 2023 print issue of Aerospace America as a Best Paper Award winner.

The AIAA’s Gas Turbine Engines Technical Committee Mechanical represents work in design, fluid mechanics and thermodynamics applied to the science and technology of air vehicle gas turbine engines and engine components.