Numerical Wing/Store Interaction Analysis of a Parametric F16 Wing
A new numerical methodology to examine fluid-structure interaction of a wing/pylon/store system has been developed. The aeroelastic equation of motion of the complete system is solved iteratively in the time domain using a two-entity numerical code comprised of ABAQUS/Standard and the Unsteady-Vort...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/29122 http://scholar.lib.vt.edu/theses/available/etd-092799-223838/ |