Drive Fan for the Icing Research Tunnel

View of the drive fan for the Icing Research Tunnel at the National Advisory Committee for Aeronautics (NACA) Aircraft Engine Research Laboratory in Cleveland, Ohio. The tunnel was built in the early 1940s to study the formation of ice on aircraft surfaces and methods of preventing or eradicating that ice. Ice buildup adds extra weight, effects aerodynamics, and sometimes blocks airflow through engines. The original 4100-horsepower induction motor was coupled directly to the 24-foot-diameter fan. The 12 wooden fan blades were protected on their leading edge by a neoprene boot. The system could create air speeds up to 300 miles per hour through the tunnel’s 6- by 9-foot test section. The large tail faring extending from the center of the fan is used to guide the airflow down the tunnel in a uniform way. A new 5000-horsepower motor was installed in 1987, and the original fan blades were replaced in 1993.

grc glenn research center drive fan drive fan research tunnel fan blades research tunnel ice aircraft engine research laboratory ice buildup national advisory committee aircraft surfaces blocks airflow induction motor engines effects aerodynamics airflow motor neoprene boot air speeds test section uniform way design nasa

1940 - 1949

NASA

https://images.nasa.gov/

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