Several improved or new techniques for propeller integration testing have been implemented at the German-Dutch Wind Tunnels (DNW). Presented here is an air-return line bridge system along with the applicable correction methodology. The implementation path followed is illustrated by the air-return line bridges systems concept validation and the systems performance validation during wind tunnel operation.
Implementation of Propeller Simulation Techniques at DNW
2006
11 Seiten
Conference paper
English
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