Tip Accelerations along X, Y Z axes

Discuss the theory and modeling of rotor aerodynamics.

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Aananthy.Sarma
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Joined: Wed Aug 01, 2018 4:17 am
Organization: Loughborough University
Location: United Kingdom

Tip Accelerations along X, Y Z axes

Postby Aananthy.Sarma » Mon Aug 20, 2018 8:19 am

Dear Dr. Jonkman,

Could you please clarify how the tip accelerations along the X, Y, Z axes are calculated? I'm using this relation to calculate the accelerations of a model turbine based on the original NREL 5MW turbine. Could you kindly let me know the equations used in the FAST estimations? I'm particularly interested in the accelerations along the flapwise direction.

Thank you!

Sincerely,

Aananthy Sarma

Jason.Jonkman
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Re: Tip Accelerations along X, Y Z axes

Postby Jason.Jonkman » Mon Aug 20, 2018 8:57 am

Dear Aananthy,

The blade-tip accelerations in the ElastoDyn module of FAST are calculated as the absolute (i.e. relative to the inertial frame) translational acceleration expressed along the local blade coordinate at the blade tip.

Best regards,
Jason Jonkman, Ph.D.
Senior Engineer | National Wind Technology Center (NWTC)

National Renewable Energy Laboratory (NREL)
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+1 (303) 384 – 7026 | Fax: +1 (303) 384 – 6901
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