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Development of modern comprehensive computer software for rotorcraft aeromechanical analysis

Narkiewicz J.

Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics

2001

nr 12

7-12

A helicopter model developed by the Helicopter Mechanics Research Group at Warsaw University of Technology is presented. The model comprises main and tail rotors, fuselage and horizontal stabiliser. The model was used for investigating an influence of various factors on helicopter and rotors motion. The sample results of calculations may be used for explanation of aeromachanical phenomena in rotorcraft.