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ICAS2014_0260: COMPUTATIONAL ANALYSIS FOR FLAPPING WING BY COUPLED CFD AND CSD SOLUTIONS
Pitch Control Law Analysis and Flight Test Demonstration of an Executive Transport Aircraft
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Communicative Action and the Network Society: A Pragmatic Marriage?
Development of Seating System with GMT for ECE 17.07 (Luggage Retention) Regulation
AIAA-2001-1244 Identification of Damages within a Plate Structure