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RotorSIM: A Coupled Multidisciplinary Simulation Integration Framework for Helicopter Rotor Blade Design

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2 Author(s)
Jian-ling Yang ; Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China ; Li-yan Zhang

Helicopter rotor blade design involves complex multidisciplinary analysis and simulation, such as aeroelastic analysis, structure analysis and dynamics simulation. In this paper, we present a simulation integration framework - RotorSIM, which integrates the analysis and simulation processes in the rotor blade design into a unique platform. The architecture, the main components, as well as the key techniques of the system, are described. A case study shows that RotorSIM can help engineers to improve their working efficiency in the blade design.

Published in:

Software Engineering, 2009. WCSE '09. WRI World Congress on  (Volume:2 )

Date of Conference:

19-21 May 2009