Paper
3 April 2008 Experimentally validated numerical analysis of aerostructures incorporating shape memory alloys
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Abstract
As the use of active structures continues to become more commercially viable, the need for accurate numerical modeling has gained importance. A current example of such a smart structure includes the variable geometry chevron. Future applications are also being designed, including a variable area jet engine nozzles and a torque tube actuators for rotor blades. This work concentrates on the FEA modeling of the Ni60Ti40 (wt %) SMA used in these applications and subsequent experimental validation. The constitutive model employed for the SMA material accounts for the full thermomechanical response and also accounts for such aspects as variable maximum transformation strain and smooth material hardening during transition. Model calibration is performed via uniaxial material testing. An overview of the model and material properties is presented followed by a discussion of the analysis results for the complex aerospace actuation applications. Comparisons to experimental validation of the overall system response are made.
© (2008) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Darren J. Hartl, Jesse T. Mooney, Dimitris C. Lagoudas, James H. Mabe, and Frederick T. Calkins "Experimentally validated numerical analysis of aerostructures incorporating shape memory alloys", Proc. SPIE 6929, Behavior and Mechanics of Multifunctional and Composite Materials 2008, 692913 (3 April 2008); https://doi.org/10.1117/12.776356
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Cited by 5 scholarly publications and 1 patent.
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KEYWORDS
Shape memory alloys

3D modeling

Calibration

Data modeling

Finite element methods

Numerical analysis

Chemical elements

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