Design of Improved and Advanced Aeroelastic Models

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Transcript of Design of Improved and Advanced Aeroelastic Models

Faculty of Engineering Department of Mechanical Engineering

ACOUSTICS & VIBRATION RESEARCH GROUP Pleinlaan 2 • B-1050 Brussel • Belgium

avrg@vub.ac.be • http://avrg.vub.ac.be

Design of improved and advanced aeroelastic models

Rasoul Shirzadeh

Design of improved and advanced aero-elastic models

Short overview of PhD topic

Acoustics & Vibration Research Group

Vrije Universiteit Brussel & Erasmushogeschool Brussel

What is Aeroelasticity?

  Aeroelasticity is the study of the interaction of inertial, structural and aerodynamic forces on aircraft, buildings, surface vehicles etc

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Acoustics & Vibration Research Group

Vrije Universiteit Brussel & Erasmushogeschool Brussel

Why is it important?

The interaction between these three forces can cause several undesirable phenomena:

o  Flutter

o  Divergence o  Limit Cycle Oscillations

o  Vortex shedding, buffeting, galloping

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Acoustics & Vibration Research Group

Vrije Universiteit Brussel & Erasmushogeschool Brussel

  Flutter (dynamic instability) is a growing oscillation of a surface leading to large amplitudes and stresses, and which can lead to structural failure

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Flutter

Example: Tacoma Narrows bridge

Acoustics & Vibration Research Group

Vrije Universiteit Brussel & Erasmushogeschool Brussel

  There are two aspects to aeroelastic models

  – A structural model   – An aerodynamic model

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Aeroelastic Model

In some cases a control model is added to represent the effects of actuators and other control elements

Acoustics & Vibration Research Group

Vrije Universiteit Brussel & Erasmushogeschool Brussel

  Simple model that can exhibit true flutter:

  Rigid wing + Springs serves as structural model

Example: Theodorsen’s model

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Flutter

Acoustics & Vibration Research Group

Vrije Universiteit Brussel & Erasmushogeschool Brussel

What we are trying to achieve?

To build better aeroelastic models by

o  Combining modal analysis and CFD (or even FSI) o  Start with simple models

o  Develop it for complex models

o  Mixed experimental-theoretical approach o  improve/update models with experimental data

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Acoustics & Vibration Research Group

Vrije Universiteit Brussel & Erasmushogeschool Brussel

Simple model 1: Vortex shedding

A. Cylinder oscillating cross flow o  To investigate frequency lock-in: discrepancies with

literature

B. Fixed cylinder o  Reynolds number = 500

o  Different turbulence models were tried.

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Acoustics & Vibration Research Group

Vrije Universiteit Brussel & Erasmushogeschool Brussel

Simple model 1: Vortex shedding

Results and open questions

o  The drag coefficients are overestimated.

o  Agreement of lift coefficients is not perfect.

o  Lock-in frequency is not consistent with literature.

o  How does OpenFOAM calculate forces? o  Which turbulence model is the best choice for our model?

o  Is Reynolds number the only parameter (or would results be different for water and air at same Re?)

o  What are the sources of these discrepancies?

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Acoustics & Vibration Research Group

Vrije Universiteit Brussel & Erasmushogeschool Brussel

Simple model 2: Theodorsen’s model

o  A rigid airfoil which is suspended by two springs, one in plunge and other one in pitch.

o  Simplest model that shows true flutter

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wingMotion tutorial case in OpenFOAM

Acoustics & Vibration Research Group

Vrije Universiteit Brussel & Erasmushogeschool Brussel

Simple model 2: Theodorsen’s model

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Questions

o  Further analysis required (amplitude, frequency, damping). Is it really flutter?

o  Understand the coding of the model in this tutorial.

Faculty of Engineering Department of Mechanical Engineering

ACOUSTICS & VIBRATION RESEARCH GROUP Pleinlaan 2 • B-1050 Brussel • Belgium

avrg@vub.ac.be • http://avrg.vub.ac.be

Any comment/suggestion?

Design of improved and advanced aero-elastic models

Thanks for your attention!