Active vibration control of cantilever beam by using optimal LQR controller von Muhammad, Hadir Abd al-Qadir, Wasmi, Hatim Rahim

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Numerical and experimental analysis of aircraft wing subjected to fatigue loading von Wasmi, Hatim Rahim, Rahim, Haydar Rad

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Study the effect of face sheets material on strength of sandwich plates with circular hole von Wasmi, Hatim Rahim, Ishaut, Nawal Falkhus

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Experimental study for materials prosthetic above knee socket under tensile or fatigue stress with varying temperatures effect von Wasmi, Hatim Rahim, Hamzah, Adawiyah Ali, Jayyad, Jumah Salman

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Aeroelastic flutter of subsonic aircraft wing section with control surface von Wasmi, Hatim Rahim, Muhaymid, Walid Jasim, Hasan, Ali Abd al-Muhsin

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Non-linear analysis of laminated composite plates under general out-of-plane loading von Wasmi, Hatim Rahim, Laftah, Muhsin Usfur, Sadiq, Ibtihal Abbas

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Analysis and performance of a proposed variable stiffness suspension system von Ubayd, Muhammad Jawad Kazim, Wasmi, Hatim Rahim

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