| Aeroelastic response and limit cycle oscillations for wing-flap-tab section with freeplay in tab WJ Al-Mashhadani, EH Dowell, HR Wasmi, AA Al-Asadi Journal of Fluids and Structures 68, 403-422, 2017 | 24 | 2017 |
| Vibration control analysis of aircraft wing by using smart material HA Abdulameer, HR Wasmi Innovative Systems Design and Engineering 6 (8), 7-42, 2015 | 17 | 2015 |
| The Modeling and Effect of FEM on Prosthetic limb H Saad, MQ Abdullah, HR Wasmi International Journal of Current Engineering and Technology 7 (3), 892-895, 2017 | 10 | 2017 |
| Experimental study for materials prosthetic above knee socket under tensile or fatigue stress with varying temperatures effect HR Wasmi, JS Chiad, AA Hamzah Journal of Engineering 20 (03), 87-95, 2014 | 8 | 2014 |
| Static & free vibration analysis of an isotropic and orthotropic thin plate using finite element analysis (FEA) EN Abbas, MQ Abdullah, HR Wasmi International Journal of Current Engineering and Technology 5 (1), 462-468, 2015 | 7 | 2015 |
| Development of Model for Creep Relaxation of Soft Gaskets in Bolted Joints at Room Temperature HR Wasmi, MQ Abdullah, OA Jassim International Journal of Current Engineering and Technology 6 (4), 2016 | 4 | 2016 |
| Finite Element Analysis and Modelling of Perlon - Fiberglass of a Prosthetic socket. HRW Hasan Saad, Mohammed Qasim Innovative Systems Design and Engineering 7 (3), 2016 | 4* | 2016 |
| Testing and estimation fatigue life of a flange connection used in power plant by ANSYS HR Wasmi, MQ Abdullah, OA Jassim International Journal of Current Engineering and Technology 6 (4), 1302-1306, 2006 | 4 | 2006 |
| Structural behaviour for composite cylindrical tank under seismic load MC Kareem, MQ Abdullah, HR Wasmi IJISET, Engineering & Technology 3 (12), 37-42, 2016 | 3 | 2016 |
| Generation and Stress Analysis in New Version of Novikov Helical Gear Combining Double Circular Arc and Crowned Involute Profiles. PDHRWPDMQA ) Mansoor Ali Innovative Systems Design and Engineering 7 (8), 2016 | 2 | 2016 |
| Numerical and experimental analysis of aircraft wing subjected to fatigue loading HR Wasmi, HR Rahim Journal of Engineering 22 (10), 62-83, 2016 | 1 | 2016 |
| Calculation of Natural Frequencies of Micro-Motor by using Finite Element Method HR Wasmi, MQ Abdullah, JM Abid, OA Jassim | | 2016 |
| Calculation of Distribution of Stress Micro Electro-Mechanical System by using Finite Element Method OAJ Mohammad Qasim Abdullah, Hatem R. Wasmi, Jasim Mohammad Abid International Journal of Current Engineering and Technology 6 (6), 2016 | | 2016 |
| BEM-FEM of Coupling for Prosthetic Socket HRW Hasan Saad, Mohammad Qasim Abdullah Innovative Systems Design and Engineering 7 (8), 2016 | | 2016 |
| Testing and Estimation Fatigue Life of a Flange Connection used in Power Plant by ANSYS OAJ Hatem R. Wasmi, Mohammad Qasim Abdullah 6 4, 2016 | | 2016 |
| Development of Model for Creep Relaxation of Soft Gaskets in Bolted Joints at Room OAJ ) Hatem R. Wasmi, Mohammad Qasim Abdullah International Journal of Current Engineering and Technology 6 (4), 2016 | | 2016 |
| Aeroelastic Flutter of Subsonic Aircraft Wing Section with Control Surface HR Wasmi, AAM Hasan, WJ Mhaimeed Journal of Engineering 21 (12), 104-123, 2015 | | 2015 |
| • Vibration-Based Terrain Analysis for Autonomous Excavator With Professor Lakmal Seneviratne DKA Dr. Hatem Rahim Wasmi IEEE, 2007 | | 2007 |
| Response of Rectangular Tank under Seismic Load by Coupling BEM and FEM MG Kareem, K Khalid, APDHR Wasmi, APDMQ Abdullah | | |
| Static and Dynamic Analysis of a vibratory bowl feeder for Automatic System PJD Dr. Hatem Rahim Wasmi, Prof. Hatem Prof. Lakmal Seneviratne | | |
