32th Congress of the International Council of the Aeronautical Sciences

10 - Safety and Security

PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVER

M. Wojtas¹, K. Raczko¹, L. Czajkowski¹; ¹Institute of Aviation, Poland

The paper discusses a prototype - Whirl Tower - test stand designed for testing rotors in the conditions of work at their nominal speed, in particular gyrocopter and helicopter rotors. The paper provides the main assumptions of the project, design steps, calculations, construction manufacturing and Whirl Tower systems test.


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