30th Congress of the International Council of the Aeronautical Sciences

02.2 - Experimental Aerodynamics

SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL

J. Cervinkaš, R. Kulhánekš, Z. Pátekš, V. Kumar, C-CADD, CSIR-NAL, India; šVZLÚ - Aerospace Research and Test Establishment, Czech Republic

Comprehensive design and development of model power unit were performed for use within low speed wind tunnel measurements to simulate full-scale propeller unit. Simultaneous research was performed to develop the methodology and the procedures leading to correct simulation of a propeller effect. Consequently, system implementation, verification and an experimental investigation were carried out.


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