Jamshid Fazilati

fazilati

 

Assistant Professor

Ph.D.  Aerospace Engineering Amirkabir University of technology, 2006-2011

Dissertation: Higher Order Finite Strip Dynamic Instability Analysis of Composite Stiffened Cylindrical Panels having Cutouts under Parametric In-plane Loads

 

M.Sc. Aerospace Engineering Amirkabir University of technology, 2003-2005

Thesis: Stability analysis of composite cylindrical panels subjected to axial loads using finite strip method

 

B.Sc. Aerospace Engineering Amirkabir University of technology, 1999-2003

Senior project: Structural Analysis of a typical composite UAV 

BSc Manufacturing Engineering Amirkabir University of technology, 2000-2006

 

 

Google scholar address 

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Web Site Address: http://ari.ac.ir/jfazilati

 


Research Interests 

  • Numerical simulation
  • Structural Stability
  • Structural mechanisms
  • Structural health monitoring

 

Publications

 Journal Papers:

1. Ovesy H.R., Fazilati J., Stability Analysis of Composite Laminated Plate and Cylindrical Shell Structures using Semi-Analytical Finite Strip Method. Composite Structures 89 (2009) 467–74.

2. Fazilati J., Ovesy H.R., Dynamic Instability Analysis of Composite Laminated Thin-Walled Structures using Two Versions of FSM. Composite Structures 92 (2010) 2060–65.

3. Fazilati J., Ovesy H.R., Boundary Condition Effects on the Parametric Stability of Moderately Thick Laminated Cylindrical Panels. Key Engineering Materials 471-472 (2011) 466-71.

4. Ovesy H.R., Fazilati J., Buckling and Free Vibration Finite Strip Analysis of Composite Plates with Cutout Based on Two Different Modeling Approaches Composite Structures, Volume 94, Issue 3, (2012), Pages 1250-1258,

5. Fazilati J., Ovesy H.R., Finite Strip Dynamic Instability Analysis of Perforated Cylindrical Shell Panels. Composite Structures, Volume 94, Issue 3, (2012), Pages 1259-1264 

6. Ovesy H.R., Fazilati J., Lay-up Effects on the Dynamic Instability of Moderately Thick Stiffened Curved Panels Applied Mechanics and Materials, 152-154, (2012) 1477

7. Ovesy H.R., Fazilati J., Parametric Instability Analysis of Moderately Thick FGM Cylindrical Panels using FSM. Computers & Structures, Volumes 108–109, October 2012, Pages 135-143. 

8. Fazilati J., Ovesy H.R., Parametric instability of laminated longitudinally stiffened curved panels with cutout using higher order FSM

Composite Structures, Volume 95, (2013) 691–696

9. Ghannadpour S.A.M, Mohammadi B., Fazilati J., Bending, buckling and vibration problems of nonlocal Euler beams using Ritz method Composite Structures, Volume 96, (2013) 584-589

10. Ovesy H.R., Fazilati J., Parametric instability analysis of laminated composite curved shells subjected to non-uniform in-plane load Composite Structures, Volume 108, (2014) 449–455.

11. Mahmoudabadi, M. R., Ovesy, H. R., Fazilati, J., Dynamic instability analysis of laminated composite cylindrical panels using the first order shear deformation layerwise theory and spline finite strip method, In Persian, J. Science and Technology of Composites, Vol. 1, No. 1, (2014) 61 -74.

12. Sharbatdar, A., Fazilati, J., Geometrically Nonlinear Analysis of Moderately Thick Curved Composite Panels under Lateral Load, In Persian, J. Science and Technology of Composites, Vol. 2, No. 1, (2015) 53-64.

13. Alisadeghi, M., Fazilati, J., Optimization of Honeycomb Impact Attenuator using Genetic Algorithm Based on Response Surface Method and Design Of Experiment; Part I: Crashworthiness, Modares Mechanical Engineering  Vol. 15, No. 12, pp. 25-36, 2015 (In Persian)

14. Alisadeghi, M., Fazilat i, J., Optimization of Honeycomb Impact Attenuator using Genetic Algorithm Based on Response Surface Method and Design of Experiment; Part II: Optimization, Modares Mechanical Engineering  Vol. 15, No. 12, pp. 37-45, 2015 (In Persian)

15. Fazilati J., Ghamarian A., Ariaeifar N.  Thin -Walled Impact Energy Absorber Optimization in Dynamic Loading  using Design Of Experiment Approach Aerospace Mechanics  Journal Vol 13, No. 1, pp 73-85, 2016 (In Persian)

16. J. Fazilati Dynamic Stability of Moderately Thick Composite Laminated Skew Plates using Finite Strip Method Mechanics of Advanced Composite Structures 2 (2015) 145-150

17. J. Fazilati, M. Alisadeghi Multiobjective Crashworthiness Optimization of Multi-Layer Honeycomb Energy Absorber Panels under Axial Impact Thin-Walled Structures 107 (2016) 197–206

18. J. Fazilati Dynamic Behavior Analysis of Moderately Thick Composite Laminated Plates Containing Square Delaminations using Spline-FSM Amirkabir Journal of Science and Technology (AJST-ME) , Accepted, d.o.i: 10.22060/MEJ.2016.792 (In Persian)

19. J. Fazilati Stability Analysis of Variable Stiffness Composite Laminated Plates With Delamination using Spline-FSM Latin American Journal of Solids and Structures 14 (2017) 528-543. 

20. A. Hadi, S. Shakhesi, H.R. Ovesy, J. Fazilati Free Vibration of FGM Cylindrical Shells on Elastic Foundation under Axial force, Lateral Pressure and Different Boundary Conditions Amirkabir Journal of Science and Technology (AJST-ME) , Accepted manuscript, 10.22060/mej.2017.12362.5319 (In Persian)

21. A. Hadi, H.R. Ovesy, S. Shakhesi, J. Fazilati, Large amplitude dynamic analysis of FGM cylindrical shells on nonlinear elastic foundation under thermomechanical loads, International Journal of Applied Mechanics (IJAM), Vol. 9(7), 1750105, 2017. (DOI: 10.1142/S1758825117501058)

22. J. Fazilati Stability Analysis of Variable Stiffness Composite Laminated Cylindrical Panels containing Delamination, Journal of Reinforced Plastics and Composites (2017) DOI: 10.1177/0731684417739988.

23. J. Fazilati, Supersonic panel flutter of curvilinear composite laminated plates in the presence of delamination, Journal of Composite Materials, 2017, (DOI: 10.1177/0021998318754641)

24. J. Fazilati, V. Khalafi, H. Shahverdi, 3-D Aero-Thermo-Elasticity Analysis of Functionally Graded Cylindrical Shell Panels, Accepted manuscript, PartG: Journal of Aerospace Engineering,

 

 Books:

 Book Chapters:

 Conference Papers:

1. Ovesy H.R., Fazilati J. Buckling Analysis of Thin-Walled Composite Cylindrical Shells Using Finite Strip Method (A Full Energy Approach) The 15th Annual (International) Conference on Mechanical Engineering (ISME), Tehran, Iran (2007).

2. Fazilati J., Ovesy H.R.  Using FSM to Predict Dynamic Instability Regions (DIR) for Thin-Walled Flat Composite Plates The 1st International Conference on Composites: Characterization, Fabrication and Application (CCFA-1) (2008).

3. Fazilati J., Ovesy H.R. Dynamic Instability Analysis of Composite Laminated Plate and Cylindrical Shell Structures Using Semi-Analytical Finite Strip Method The 7th International Conference on Composite Science and Technology (ICCST/7), Sharjah, UAE (2009).

4. Fazilati J., Ovesy H.R. Prediction of the Dynamic Behavior of Functionally Graded Thin Cylindrical Shells Using Finite Strip Method 17th. Annual (International) Conference on Mechanical Engineering (ISME), University of Tehran, Iran (2009).

5. Fazilati J., Ovesy H.R. Dynamic Stability of Laminated Cylindrical Shells Based on a Higher-Order Shear Deformation Theory using FSM IJSSD Symposium; Progress in Structural Stability and Dynamics, Hong Kong, Hong Kong (2009).

6. Fazilati J., Ovesy H.R. Dynamic Stability of FGM Cylindrical Shells Based on Higher-Order Theory using FSM Tenth International Conference on Computational Structures Technology (CST2010), Valencia, Spain (2010).

7. Fazilati J., Ovesy H.R. Boundary Condition Effects on the Parametric Stability of Moderately Thick Laminated Cylindrical Panels  8th Int. Conf. on Composite Science and Technology (ICCST/8), Malaysia (2011).

8. Ovesy H.R., Fazilati J. Buckling and Free Vibration Finite Strip Analysis of Composite Plates with Cutout Based on Two Different Modeling Approaches 16th Int. Conf. on Composite Structures (ICCS-16), Porto, Portugal (2011).

9. Fazilati J., Ovesy H.R. Finite Strip Dynamic Instability Analysis of Perforated Cylindrical Shell Panels 16th Int. Conf. on Composite Structures (ICCS-16), Porto, Portugal (2011).

10. Ovesy H.R., Fazilati J. Parametric Instability Analysis of Laminated Flat and Cylindrical Panels Subjected to Non-Uniform In-Plane Loads 17th Int. Conf. on Composite Structures (ICCS-17), Porto, Portugal (2013).

11. Ovesy H.R., Fazilati J., M. R. Mahmoudabadi Finite strip buckling and free vibrations analysis of laminated composite plates containing delamination using a first order layerwise theory 12th Int. Conf. on Computational Structures Technology (CST-2014), Naples, Italy (2014).

12. A. Hadi, H.R. Ovesy, S. Shakhesi, J. Fazilati The Effects of Kinematic Relations and Inertia on Free Vibration of Cylindrical Shells 14th Conf. of Iranian Aerospace Society (Aero2015), Tehran (2015).

13. A. Hadi, H.R. Ovesy, S. Shakhesi, J. Fazilati The Effects of Inertia and Different Shell Theories on The Vibration Characteristics of Cylindrical Shells 23rd Annual Int. Conference on Mechanical Engineering (ISME2015), Tehran, Iran. (2015).

14. V. Khalafi, J. Fazilati Supersonic Flutter Analysis of Curvilinear Fiber Variable Stiffness Composite Laminated Plates 5th International Conference on Composites: Characterization, Fabrication and Application (CCFA-5), 2016 

15. J. Fazilati, Higher Order FSM Stability Analysis of Curved VSCL Panels Containing Geometrical Defects, 20th International Conference on Composite Structures (ICCS20), 2017, Paris, France

16. V. Khalafi, J. Fazilati, Panel Flutter Analysis of Moderately Thick Variable Stiffness Composite Laminated Plates using Isogeometric Analysis, 20th International Conference on Composite Structures (ICCS20), 2017, Paris, France

17. V. Khalafi, J. Fazilati, Free Vibration Analysis of VSCL Thin Plates Using IGA, 7th International Conference on Acoustics and Vibration (ISAV2017), Tehran, Iran

18. A Hadi, HR Ovesy, S Shakhesi, J Fazilati, Thermal Induced Vibration of FGM Cylindrical Shell on Elastic foundation, 7th International Conference on Acoustics and Vibration (ISAV2017) , Tehran, Iran

 

Teaching Experiences

  • advanced engineering mathematics I & II
  • Theory of Plates and Shells
  • Fatigue and Fracture
  • Mechanical behavior of Materials
  • Advanced engineering numerical analysis
  • Orbital Mechanics 
  • Computer Programming using FORTRAN
  • Material Strength Lab.

 

Research Supervision

  • M. Alisadeghi, Analysis of Multi-layered Honeycomb Energy Absorbing Structure under Impact Loads, MSc Thesis, 2015.
  • Sharbatdar, Nonlinear Post-buckling analysis of double curvature shells in mechanical loading, MSc thesis, 2014.
  • H. Shirmohammadali, Buckling Analysis of Perforated Composite Thin Panel with the Spline Finite Strip Method, 2013.
  • M.R. Mahmoudabadi, , Finite Strip Analysis of the Dynamic Instability of Laminated Composite Cylindrical Shells with Delaminations under Parametric Harmonic, MSc thesis, 2014.
  • M.S. Namavar, post-buckling analysis of perforated composite thin panel with the spline finite strip method, MSc thesis, 2015.

 

 

 

Professional Experiences

  • HF Dorna Co.,  aeroelasticity and structural design studies
  • Farnaas Project, the first Iranian human-powered plane, structural design studies and engineering.
  • Raha Air and Space Co., think-tanking and future planning studies.
  • Tadbir Sanat Co., engineering activities in the field of steel briquetting and machine vision.
  • Nirou Research Institute, engineering activities in the field of switch reluctance motors design.
  • Aerospace Research Institute, Shock absorber and energy attenuator design.

 

 

 

 
 
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