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  1. 1
    Subsonic Aeroelastic Analysis of a Thin Flat Plate
    “... vibration input, obtained using MSC-NASTRAN, a finite element code. The flutter equation was obtained using...”
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  2. 2
    Aeroelastic Tailoring Of Woven Cantilevered Glass-Epoxy Plate-Like Aircraft Wing
    “... were also conducted using MSc.Nastran structural analysis in conjunction with ZAERO’s flutter program...”
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