51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR&amp;gt; 18th AIAA/ASME/AHS Adap 2010
DOI: 10.2514/6.2010-2953
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High-Fidelity Flutter Analysis of a Re-Usable Launch Demonstrator with Wing-Tip Vertical Tails

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