بیژن محمدی
رتبه علمی: استادیار
پست الکترونیکی: bijan_mohammadi @ iust.ac.ir
آدرس: دانشکده مهندسی مکانیک، دانشگاه علم و صنعت ایران، نارمک، تهران، ایران
دانشگاه های محل تحصیل
- دکترا، دانشگاه صنعتی امیرکبیر، ایران
- فوق لیسانس، دانشگاه صنعتی امیرکبیر ، ایران
- لیسانس، دانشگاه صنعتی امیرکبیر ، ایران
زمینه های تحقیقاتی
- مکانیک خرابی محیط های پیوسته محلی
- مکانیک خرابی محیط های پیوسته غیر-محلی
- مکانیک شکست محاسباتی
- آنالیز خرابی در مواد مرکب چندلایه
- پایداری سازه های هوایی
- تحلیل و طراحی سازه های هوایی
- تحلیل و طراحی سازه ماهواره
آزمایشگاه تحقیقاتی سازه های هوایی
- Damage in Composite Materials (Iran Univ. of Science & Tech.) (MSc & PhD)
- Damage in Composite Materials (Amirkabir Univ. of Tech.) (PhD)
- Micromechanics (Shahid Rajaee Teacher Training Univ.) (PhD)
- Advanced Aircraft Structural Analysis (Iran Univ. of Science & Tech.) (MSc)
- Finite Element Method (Iran Univ. of Science & Tech.) (MSc)
- Advanced Spacecraft Structural Design (Iran Univ. of Science & Tech.) (MSc)
- Fatigue-Fracture & Creep (Shahid Beheshti University) (MSc)
- Aircraft Structural Analysis (Amirkabir Univ. of Tech.) (BSc)
- Aircraft Structural Design (Amirkabir Univ. of Tech.) (BSc)
- Engineering Mechanics - Static (Amirkabir Univ. of Tech.) (BSc)
- Engineering Mechanics - Static (Iran Univ. of Science & Tech.) (BSc)
توسعه نرم افزار
- توسعه نرم افزار جامع تحلیل و ارزیابی عمر خستگی سازه های فلزی
- توسعه نرم افزار رشد ترک خستگی در صفحات فلزی
- توسعه نرم افزار جامع بارگذاری سازه هواپیماهای رده 23 و 25 استانداردهای صلاحیت پرواز هوایی
فعالیتهای پژوهشی- صنعتی
- طراحی و ساخت نمونه مهندسی لبه حمله کامپوزیتی یک بال مجهز به سیستم مقابله با یخِ الکتروترمال
- طراحی و تحلیل ارابه فرود ثابت هواپیمای دونفره تمام کامپوزیتی
- طراحی و تحلیل سازه بال یک پرنده تمام کامپوزیتی با نسبت منظری بالا
- ترمیم کامپوزیتی و افزایش عمر سازه اسپار فلزی اصلی یک جنگنده
- پایش رشد ترک در یک نمونه فلزی به روش امپدانس الکترومکانیکی
- طراحی، ساخت و تست یک پایه موتور فلزی پیچیده
- طراحی تا نظارت بر ساخت ارابههای فرود Oleo یک پرنده
- طراحی تا نظارت بر ساخت استند اندازهگیری مرکز ثقل یک پرنده
- تحلیل آسیب در صفحات کامپوزیتی چندلایه با استفاده از مکانیک خرابی- پلاستیسیته محیطهای پیوسته
- تحلیل خرابی صفحات کامپوزیتی چند لایه با استفاده از کوپل تئوری های خرابی مقیاس میکرو- مزو
- شبیهسازی جدایی اتصال وصله کامپوزیتی از پانلهای آلومینیومی حاوی ترک
- بررسی رفتار پس از کمانش صفحات کامپوزیتی چند لایه حاوی جدایی بین لایه ای
- تحلیل رشد ترک در پانل های نازک با استفاده از روش المان محدود توسعه یافته
- تحلیل خستگی ریشه پره توربین بادی کیلوواتی با استفاده از المان واسط چسبنده
- پیش بینی عمر خستگی چندلایه کامپوزیتی با استفاده از روش مکانیک خرابی پبوسته
- تأثیر مکانیزمهای ثانویه آسیب در خواص شکست بینلایهای کامپوزیتهای چندلایه
- بررسی خواص شکست ماده نانوساختار شده تحت فرآیند پرسکاری شیار مقید
- بررسی خواص شکست در مواد نانو ساختار شده در فرآیند ECAP
آموزش نرم افزار های تخصصی
مقالات مجلات معتبر
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1. D. Salimi-Majd, F. Shahabi, B. Mohammadi: Effective local stress intensity factor criterion for prediction of crack growth trajectory under mixed mode fracture conditions. Theoretical and Applied Fracture Mechanics 01/2016; DOI:10.1016/j.tafmec.2016.01.009. 2. A. Farrokhabadi, B. Mohammadi, H. Hosseini-Toudeshky: A generalized plane-strain crack density based model for evaluating the finite fracture toughness of composite laminates. Mechanics of Advanced Materials and Structures 11/2015; DOI:10.1080/15376494.2015.1120906. 3. D. Salimi-Majd, V. Azimzadeh, B. Mohammadi: Loading Analysis of Composite Wind Turbine Blade for Fatigue Life Prediction of Adhesively Bonded Root Joint. Applied Composite Materials 06/2015; 22:269–287; DOI:10.1007/s10443-014-9405-4. 4. A. Farrokhabadi, B. Mohammadi, H. Hosseini-Toudeshky: A simplified micromechanics model for predicting the stiffness degradation in symmetric composite laminates. Fatigue & Fracture of Engineering Materials & Structures 05/2015; 38(11); DOI:10.1111/ffe.12306. 5. B. Mohammadi, F. Shahabi: On computational modeling of postbuckling behavior of composite laminates containing single and multiple through-the-width delaminations using interface elements with cohesive law. Engineering Fracture Mechanics 04/2015; DOI:10.1016/j.engfracmech.2015.04.005 6. M. Haghbeigi, E. Badrikouhi, B. Mohammadi: Dynamic Analysis and Simulation of an Aircraft Landing Gear System. 7. B. Mohammadi, M. Tavoli, F. Djavanroodi: Effects of Constrained Groove Pressing (CGP) on the plane stress fracture toughness of pure copper. Structural Engineering & Mechanics 12/2014; 52(5):957-969. DOI:10.12989/sem.2014.52.5.957. 8. M. Jalalvand, M. R. Wisnom, H. Hosseini-Toudeshky, B. Mohammadi: Experimental and numerical study of oblique transverse cracking in cross-ply laminates under tension. Composites Part A Applied Science and Manufacturing 12/2014; 67:140–148. DOI:10.1016/j.compositesa.2014.08.004. 9. M. Hajikazemi, M.H. Sadr, H. Hosseini-Toudeshky, B. Mohammadi: Thermo-elastic constants of cracked symmetric laminates: A refined variational approach. International Journal of Mechanical Sciences 12/2014; 89:47–57. DOI:10.1016/j.ijmecsci.2014.08.008. 10. B. Mohammadi, Hamed Olia, H. Hosseini-Toudeshky: Intra and damage analysis of laminated composites using coupled continuum damage mechanics with cohesive interface layer. Composite Structures 10/2014; 120. DOI:10.1016/j.compstruct.2014.10.004. 11. G. Sadeghi, H. Hosseini-Toudeshky, B. Mohammadi: In‐plane progressive matrix cracking analysis of symmetric cross‐ply laminates with holes. Fatigue & Fracture of Engineering Materials & Structures 03/2014; 37(3). DOI:10.1111/ffe.12113. 12. G. Sadeghi, H. Hosseini-Toudeshky, B. Mohammadi: An investigation of matrix cracking damage evolution in composite laminates - Development of an advanced numerical tool. Composite Structures 02/2014; 108(1):937-950. DOI:10.1016/j.compstruct.2013.10.007. 13. B. Mohammadi, D. Salimi-Majd: Investigation of delamination and damage due to free edge effects in composite laminates using cohesive interface elements. 01/2014; 2(2):101-118. DOI:10.5267/j.esm.2014.2.001. 14. H. Hosseini-Toudeshky, M. S. Goodarzi, B. Mohammadi: Prediction of through the width delamination growth in post-bukled laminates under fatigue loading using de-cohesive law. Structural Engineering & Mechanics 10/2013; 48(1). DOI:10.12989/sem.2013.48.1.041. 15. H. Hosseini-Toudeshky, Ali Jasemzadeh, B. Mohammadi: Investigation of effective parameters on composite patch debonding under static and cyclic loading using cohesive elements. Finite Elements in Analysis and Design 10/2013; 74:67–75. DOI:10.1016/j.finel.2013.06.003. 16. H. Hosseini-Toudeshky, B. Mohammadi, Pooya Saniei: Fatigue Multi-Cracks Growths in Plates Using J-Integral Approach with a Developed Home FEM Software. Key Engineering Materials 07/2013; 560:61-70. DOI:10.4028/www.scientific.net/KEM.560.61. 17. M. Jalalvand, H. Hosseini-Toudeshky, B. Mohammadi: Numerical modeling of diffuse transverse cracks and induced delamination using cohesive elements. ARCHIVE Proceedings of the Institution of Mechanical Engineers Part C Journal of Mechanical Engineering Science 1989-1996 (vols 203-210) 07/2013; 227(7):1392-1405. DOI:10.1177/0954406212460974. 18. H. Hosseini-Toudeshky, M. A. Ghaffari, B. Mohammadi: Mixed-mode crack propagation of stiffened curved panels repaired by composite patch under combined tension and shear cyclic loading. Aerospace Science and Technology 07/2013; 28(1):344–363. DOI:10.1016/j.ast.2012.12.001. 19. M. Jalalvand, H. Hosseini-Toudeshky, B. Mohammadi: Homogenization of diffuse delamination in composite laminates. Composite Structures 06/2013; 100:113–120. DOI:10.1016/j.compstruct.2012.12.022. 20. S.A.M. Ghannadpour, B. Mohammadi, J. Fazilati: Bending, buckling and vibration problems of nonlocal Euler beams using Ritz method. Composite Structures 02/2013; 96:584–589. DOI:10.1016/j.compstruct.2012.08.024. 21. H. Hosseini-Toudeshky, M.A. Ghaffari, B. Mohammadi: Composite Repair of Curved Stiffened Aluminum Panels under Combined Tension and Shear Cyclic Loadings. Applied Mechanics and Materials 11/2012; 225:219-224. DOI:10.4028/www.scientific.net/AMM.225.219. 22. H. Hosseini-Toudeshky, M. S. Goodarzi, B. Mohammadi: Multiple Delaminations Growth in Composite Laminates under Compressive Cyclic Loading in Post-Buckling. Applied Mechanics and Materials 11/2012; 225:195-200. DOI:10.4028/www.scientific.net/AMM.225.195. 23. H. Hosseini-Toudeshky, A. Farrokhabadi, B. Mohammadi: Implementation of a micro-meso approach for progressive damage analysis of composite laminates. Structural Engineering & Mechanics 09/2012; 43(5). DOI:10.12989/sem.2012.43.5.657. 24. H. Hosseini-Toudeshky, A. Farrokhabadi, B. Mohammadi: Consideration of concurrent transverse cracking and induced delamination propagation using a generalized micro‐meso approach and experimental validation. Fatigue & Fracture of Engineering Materials & Structures 09/2012; 35(9). DOI:10.1111/j.1460-2695.2012.01674.x. 25. B. Mohammadi, F. Shahabi: The effect of edge delamination onset and growth on the post buckling behavior of laminated composites by using de-cohesive elements. 26. A. Farrokhabadi, H. Hosseini-Toudeshky, B. Mohammadi: Development of a Damage Analysis Method in Laminated Composites Using Finite Fracture Toughness of Single Lamina. Mechanics of Advanced Materials and Structures 01/2012; 20(3). DOI:10.1080/15376494.2011.584144. 27. B. Mohammadi, F. Shahabi, S. A. M. Ghannadpou: Post-buckling delamination propagation analysis using interface element with de-cohesive constitutive law. Procedia Engineering 12/2011; 10:1801-1806. DOI:10.1016/j.proeng.2011.04.299. 28. B. Mohammadi, S. A. M. Ghannadpour: Energy approach vibration analysis of nonlocal Timoshenko beam theory. Procedia Engineering 12/2011; 10:1770-1775. DOI:10.1016/j.proeng.2011.04.294. 29. H. Hosseini-Toudeshky, A. Farrokhabadi, B. Mohammadi: Analysis of damage events in quasi-isotropic laminates using a generalized micromechanics approach. Procedia Engineering 12/2011; 10:236-241. DOI:10.1016/j.proeng.2011.04.042. 30. H. Hosseini-Toudeshky, M.A. Ghaffari, B. Mohammadi: Fatigue propagation of induced cracks by stiffeners in repaired panels with composite patches. Composite Structures 12/2011; 10(5):3293-3298. DOI:10.1016/j.proeng.2011.04.542. 31. H. Hosseini-Toudeshky, Ali Jasemzadeh, B. Mohammadi: Fatigue Debonding Analysis of Repaired Aluminium Panels by Composite Patch using Interface Elements. Applied Composite Materials 12/2011; 18(6):571-584. DOI:10.1007/s10443-011-9229-4. 32. H. Hosseini-Toudeshky, A. Farrokhabadi, B. Mohammadi: Progressive Damage Analyses of Composite Laminates Exhibiting Free Edge Effects Using a New Micro-Meso Approach. Key Engineering Materials 02/2011; 471-472:263-267. DOI:10.4028/www.scientific.net/KEM.471-472.263. 33. S.A.M. Ghannadpour, B. Mohammadi: Vibration of Nonlocal Euler Beams Using Chebyshev Polynomials. Key Engineering Materials 02/2011; 471-472:1016-1021. DOI:10.4028/www.scientific.net/KEM.471-472.1016. 34. H. Hosseini-Toudeshky, A. Jasemzadeh, B. Mohammadi: Fatigue Delamination Analysis of Composite Laminates with a Central Hole Using Interface Elements. Key Engineering Materials 02/2011; 471-472:568-571. DOI:10.4028/www.scientific.net/KEM.471-472.568. 35. A. Farrokhabadi, H. Hosseini-Toudeshky, B. Mohammadi: A generalized micromechanical approach for the analysis of transverse crack and induced delamination in composite laminates. Composite Structures 01/2011; 93(2):443-455. DOI:10.1016/j.compstruct.2010.08.036. 36. H. Hosseini-Toudeshky, M. Karimi, B. Mohammadi: Acoustic Fatigue Crack Growth Prediction in Coupled Air Structures. Key Engineering Materials 11/2010; 452-453:293-296. DOI:10.4028/www.scientific.net/KEM.452-453.293. 37. H. Hosseini-Toudeshky, B. Mohammadi: Coupling of Continuum Damage Mechanics with De-Cohesive Element for Delamination Analysis in Laminated Composites. Advanced Materials Research 08/2010; 123-125:527-530. DOI:10.4028/www.scientific.net/AMR.123-125.527. 38. S.A.M. Ghannadpour, B. Mohammadi: Buckling Analysis of Micro and Nano-Rods/Tubes Based on Nonlocal Timoshenko Beam Theory Using Chebyshev Polynomials. Advanced Materials Research 08/2010; 123-125:619-622. DOI:10.4028/www.scientific.net/AMR.123-125.619. 39. H. Hosseini-Toudeshky, F. Mazaheri Torei, B. Mohammadi: Progressive Damage Analysis of Laminated Composites Using Element Free Galerkin Method. Advanced Materials Research 08/2010; 123-125:579-582. DOI:10.4028/www.scientific.net/AMR.123-125.579. 40. H. Hosseini-Toudeshky, S. Hosseini, B. Mohammadi: Delamination buckling growth in laminated composites using layerwise-interface element. Composite Structures 07/2010; 92(8):1846-1856. DOI:10.1016/j.compstruct.2010.01.013. 41. A. Farrokhabadi, H. Hosseini-Toudeshky, B. Mohammadi: Damage analysis of laminated composites using a new coupled micro‐meso approach. Fatigue & Fracture of Engineering Materials & Structures 04/2010; 33(7):420 - 435. DOI:10.1111/j.1460-2695.2010.01456.x. 42. H. Hosseini-Toudeshky, Saman Hosseini, B. Mohammadi: Progressive delamination growth analysis using discontinuous layered element. Composite Structures 03/2010; 92(4):883-890. DOI:10.1016/j.compstruct.2009.09.028. 43. B. Mohammadi, H. Hosseini-Toudeshky, M.H. Sadr-Lahidjani: Failure analysis of laminates by implementation of continuum damage mechanics in layer-wise finite element theory. Structural Engineering & Mechanics 12/2009; 33(6). DOI:10.12989/sem.2009.33.6.657. 44. H. Hosseini-Toudeshky, B. Mohammadi: Mixed-Mode Experimental Fatigue Crack Growth Analyses of Thin Aluminum Panels Repaired with Composite Patches. Composite Structures 11/2009; 91(1):1-8. DOI:10.1016/j.compstruct.2009.04.022. 45. H. Hosseini-Toudeshky, M. Jalalvand, B. Mohammadi: Delamination analysis of holed composite laminates using interface elements. Procedia Engineering 07/2009; 1(1):39-42. DOI:10.1016/j.proeng.2009.06.011. 46. H. Hosseini-Toudeshky, A. Farrokhabadi, B. Mohammadi: Transverse crack density evolution in a single orthotropic lamina under multi-axial stresses using analytical method. Procedia Engineering 07/2009; 1(1):109-112. DOI:10.1016/j.proeng.2009.06.026. 47. H. Hosseini-Toudeshky, B. Mohammadi: Thermal residual stresses effects on fatigue crack growth of repaired panels bounded with various composite materials. Composite Structures 06/2009; 89(2):216-223. DOI:10.1016/j.compstruct.2008.07.029. 48. H. Hosseini-Toudeshky, S. Hosseini, B. Mohammadi: Buckling and Delamination Growth Analysis of Composite Laminates Containing Embedded Delaminations. Applied Composite Materials 04/2009; 17(2):95-109. DOI:10.1007/s10443-009-9092-8. 49. B. Mohammadi, H Hosseini-Toudeshky, M-H Sadr-Lahidjani: Free-edge effects analysis of angle-ply laminates under transverse loading using layer-wise finite-element method with semi-analytical shear stress calculation. ARCHIVE Proceedings of the Institution of Mechanical Engineers Part C Journal of Mechanical Engineering Science 1989-1996 (vols 203-210) 02/2009; 223(2):293-306. DOI:10.1243/09544062JMES1063. 50. H. Hosseini-Toudeshky, M. Saber, B. Mohammadi: Finite element crack propagation of adhesively bonded repaired panels in general mixed-mode conditions. Finite Elements in Analysis and Design 01/2009; 45(2):94-103. DOI:10.1016/j.finel.2008.07.010. 51. B. Mohammadi, H. Hosseini-Toudeshky, M. H. Sadr-Lahidjani: Progressive damage analysis of angle-ply laminates exhibiting free edge effects continuum damage mechanics with layer-wise finite element method. Fatigue & Fracture of Engineering Materials & Structures 08/2008; 31(7):549 - 568. DOI:10.1111/j.1460-2695.2008.01242.x. 52. H. Hosseini-Toudeshky, B. Mohammadi, S. Bakhshandeh: Crack trajectory analysis of single-side repaired thin panels in mixed-mode conditions using glass/epoxy patches. Computers & Structures 05/2008; 86(9-86):997-1005. DOI:10.1016/j.compstruc.2007.04.015. 53. H. Hosseini-Toudeshky, M. Saber, B. Mohammadi: Mixed-mode 3-D crack propagation of repaired thin aluminum panels using single-side composite patches. International Journal of Fracture 01/2008; 153(2):105-116. DOI:10.1007/s10704-008-9303-6. 54. B. Mohammadi, H. Hosseini-Toudeshky, M. H. Sadr-Lahidjani, Shahram Aivazzadeh: Prediction of Inelastic Behavior of Composite Laminates Using Multi-Surface Continuum Damage-Plasticity. Advanced Materials Research 01/2008; 47-50:773-776. DOI:10.4028/www.scientific.net/AMR.47-50.773. 55. H. Hosseini-Toudeshky, M. Saber, B. Mohammadi: Real 3D Crack-Front and Crack Trajectory Analyses of Single-Side Repaired Thick Aluminium Panels. Advanced Materials Research 01/2008; 47-50:777-780. DOI:10.4028/www.scientific.net/AMR.47-50.777. 56. H. Hosseini-Toudeshky, M. Jalalvand, B. Mohammadi: Delamination of Laminates Governed by Free Edge Interlaminar Stresses Using Interface Element. Key Engineering Materials 01/2008; 385-387:821-824. DOI:10.4028/www.scientific.net/KEM.385-387.821. 57. B. Mohammadi, H. Hosseini-Toudeshky, M. H. Sadr-Lahidjani: Damage Evolution of Laminated Composites Using Continuum Damage Mechanics Incorporate with Interface Element. Key Engineering Materials 01/2008; 385-387:277-280. DOI:10.4028/www.scientific.net/KEM.385-387.277. 58. H. Hosseini-Toudeshky, M. Shamboli, B. Mohammadi: Experimental Investigations on the Effects of Thermal Residual Stresses on the Efficiency of Repaired Panels with Glass/Epoxy Composite Patch. Key Engineering Materials 01/2008; 385-387:141-144. DOI:10.4028/www.scientific.net/KEM.385-387.141. 59. H. Hosseini-Toudeshky, B. Mohammadi: A simple method to calculate the crack growth life of adhesively repaired aluminum panels. Composite Structures 07/2007; 79(2-79):234-241. DOI:10.1016/j.compstruct.2006.01.005. 60. H. Hosseini-Toudeshky, B. Mohammadi, S. Bakhshandeh: Mixed‐mode fatigue crack growth of thin aluminium panels with single‐side repair using experimental and numerical methods. Fatigue & Fracture of Engineering Materials & Structures 06/2007; 30(7):629 - 639. DOI:10.1111/j.1460-2695.2007.01142.x. 61. H. Hosseini-Toudeshky, B. Mohammadi, G. Sadeghi, H.R. Daghyani: Numerical and experimental fatigue crack growth analysis in mode-I for repaired aluminum panels using composite material. Composites Part A Applied Science and Manufacturing 04/2007; 38(4):1141-1148. DOI:10.1016/j.compositesa.2006.06.003. 62. S.A.M. Ghannadpour, A. Najafi, B. Mohammadi: On the buckling behavior of cross-ply laminated composite plates due to circular/elliptical cutouts. Composite Structures 09/2006; 75(s 1–4):3–6. DOI:10.1016/j.compstruct.2006.04.071. 63. B. Mohammadi, A. Najafi, S. A. M. Ghannadpour: Effective widths of compression-loaded of perforated cross-ply laminated composites. Composite Structures 09/2006; 75(1):7-13. DOI:10.1016/j.compstruct.2006.04.025. 64. H. Hosseini-Toudeshky, S. Bakhshandeh, B. Mohammadi, H.R. Daghyani: Experimental investigations on fatigue crack growth of repaired thick aluminium panels in mixed-mode conditions. Composite Structures 09/2006; 75(1):437-443. DOI:10.1016/j.compstruct.2006.04.021 65. H. Hosseini-Toudeshky, B. Mohammadi, B. Hamidi, H.R. Ovesy: Analysis of composite skin/stiffener debounding and failure under uniaxial loading. Composite Structures 09/2006; 75(1):428-436. DOI:10.1016/j.compstruct.2006.04.019. 66. H. Hosseini-Toudeshky, B. Mohammadi, Hamid Reza Daghyani: Mixed-mode fracture analysis of aluminium repaired panels using composite patches. Composites Science and Technology 02/2006; 66(2):188-198. DOI:10.1016/j.compscitech.2005.04.028. 67. M Sedighi, B. Mohammadi: On the static and dynamic analysis of a small satellite (MESBAH). Acta Astronautica 05/2003; 52(9). DOI:10.1016/S0094-5765(03)00083-3. |
دروس ارائه شده
- Damage in Composite Materials (Iran Univ. of Science & Tech.) (MSc & PhD)
- Damage in Composite Materials (Amirkabir Univ. of Tech.) (PhD)
- Micromechanics (Shahid Rajaee Teacher Training Univ.) (PhD)
- Advanced Aircraft Structural Analysis (Iran Univ. of Science & Tech.) (MSc)
- Finite Element Method (Iran Univ. of Science & Tech.) (MSc)
- Advanced Spacecraft Structural Design (Iran Univ. of Science & Tech.) (MSc)
- Fatigue-Fracture & Creep (Shahid Beheshti University) (MSc)
- Aircraft Structural Analysis (Amirkabir Univ. of Tech.) (BSc)
- Aircraft Structural Design (Amirkabir Univ. of Tech.) (BSc)
- Engineering Mechanics - Static (Amirkabir Univ. of Tech.) (BSc)
- Engineering Mechanics - Static (Iran Univ. of Science & Tech.) (BSc)