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Richard Bennett


Last seen: 2 years ago Active since 2012

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Time history solution of finite element structrual dynamic problem using methods other than the modal technique.
The time history solution for the aeroelastic response of helicopter requires several finite elements to capture the coupling ef...

8 years ago | 0 answers | 0

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Simulink Xplane Connection
I am developing some new control laws for novel types of rotorcraft. Naturally I am using Simulink for developing the control ...

12 years ago | 1 answer | 0

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