Aeroelastic Response of Composite High-Speed Rotorcraft Blade with Non-uniform Cross Section in Unsteady Subsonic Compressible Flow
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Aeroelastic Response of Composite High-Speed Rotorcraft Blade with Non-uniform Cross Section in Unsteady Subsonic Compressible Flow
Authors / Details: Jaber Javanshir Hasbestan, National Center for Computational Engineering, Touraj Farsadi, METU universityRecently Viewed Items
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