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آدرس: تهران، میدان رسالت، خیابان هنگام، دانشگاه علم و صنعت ایران، دانشکده مهندسی مکانیک

کدپستی: 13114-16846

صندوق پستی: 163-16765

تلفن:9-77491228

فاکس:77240488

پست الکترونیکی:

meresearch@iust.ac.ir

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قطب علمی مکانیک جامدات تجربی و دینامیک

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کادمان

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کانون دانش آموختگان و اساتید دانشکده مهندسی مکانیک دانشگاه علم و صنعت ایران

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:: بیژن محمدی ::

  نام: دکتر بیژن محمدی

  رتبه علمی: دانشیار

  تلفن: مستقیم                77240208 

  تلفن: عمومی                50-77240540   داخلی: 2967

  فاکس: 77240488

  پست الکترونیکی: bijan_mohammadi  iust.ac.ir

  صفحه الکترونیکیhttp://webpages.iust.ac.ir/Bijan_Mohammadi

  آدرس: دانشکده مهندسی مکانیک، دانشگاه علم و صنعت ایران، نارمک، تهران، ایران

http://www.iust.ac.ir/find.php?item=16.9924.16566.en

دانشگاه های محل تحصیل

  • دکترا، دانشگاه صنعتی امیرکبیر، ایران
  • فوق لیسانس، دانشگاه صنعتی امیرکبیر ، ایران
  • لیسانس، دانشگاه صنعتی امیرکبیر ، ایران


  زمینه های پژوهشی-صنعتی

 
  • آنالیز خرابی در چند لایه های کامپوزیتی به روش های:
    • مکانیک خرابی محیط ­های پیوسته
    • مایکرومکانیک خرابی
    • مزومکانیک
  • کمانش و پس از کمانش سازه های کامپوزیتی
  • طراحی سازه ­هواپیمای فلزی و کامپوزیتی
  • بارگذاری هواپیما بر اساس استاندارد Part 23 و Part 25
  • طراحی و ساخت انواع ارابه های فرود oleo هواپیماهای سبک
  • طراحی و ساخت انواع ارابه های فرود کامپوزیتی هواپیماهای سبک
  • ارزیابی و تخمین عمر توربین گاز
    • تحلیل خستگی کم چرخه
    • تحلیل خزش
    • تحلیل خستگی ترمومکانیکی
    • تحلیل سایش
    • تحلیل فرسایش
    • تحلیل خوردگی تنشی
    • تحلیل خوردگی گرم
    • تحلیل خوردگی اکسیدیشین

 
دانشجویان تحت سرپرستی

آزمایشگاه تحقیقاتی سازه و سیستم های هوایی

آزمایشگاه تحقیقاتی سازه­ و سیستم­های هوایی در دانشکده مهندسی مکانیک دانشگاه علم و صنعت ایران، یکی از آزمایشگاهی تازه تاسیسی است که با توجه به توانمندی­‌های علمی، سوابق اجرایی موفق صنعتی، و دراختیار داشتن تیم­‌های تخصصی توانمند، می­‌تواند در آینده در نوع خود در کشور کم نظیر باشد و فضای مناسبی را جهت انجام تحقیقات و پروژه­ های تحقیقاتی- صنعتی در حوزه تحلیل، طراحی و ساخت سازه­ و سیستم­ های هوایی و تخمین عمر سازه­‌های هوایی فراهم نماید.

دروس: 

  • 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

  • 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 بین­ لایه­ ای کامپوزیت‏ های چندلایه

  • بررسی خواص شکست ماده نانوساختار شده تحت فرآیند پرسکاری شیار مقید

  • بررسی خواص شکست در مواد نانو ساختار شده در فرآیند ECAP                                                                              

مقالات مجلات معتبر 

  1. Mohammadi, B., Pourhosseinshahi, M., Sohrabi, A., & Fard, A. H. K. (2020). A new FE modeling procedure to investigate the effects of toughening mechanisms on the fracture toughness of laminated composites. Theoretical and Applied Fracture Mechanics, 102507. DOI: 10.1016/j.tafmec.2020.102507.
  2. Pakdel, H., Mohammadi, B., & Hosseini-Toudeshky, H. (2020). Stress and energy based prediction of crack distribution pattern in general cross-ply laminates. Engineering Fracture Mechanics, 223, 106769.‏ DOI: 10.1016/j.engfracmech.2019.106769.
  3. Mahmoudi, A., & Mohammadi, B. (2019). On the evaluation of damage-entropy model in cross-ply laminated composites. Engineering Fracture Mechanics, 219, 106626. DOI: 10.1016/j.engfracmech.2019.106626.
  4. Mahmoudi, A., & Mohammadi, B. (2019). Theoretical-experimental investigation of temperature evolution in laminated composites due to fatigue loading. Composite Structures, 225, 110972. DOI: 10.1016/j.compstruct.2019.110972.
  5. Khoddami, A., Salimi-Majd, D., & Mohammadi, B. (2019). Finite element and experimental investigation of multiple solid particle erosion on Ti-6Al-4V titanium alloy coated by multilayer wear-resistant coating. Surface and Coatings Technology, 372, 173-189. DOI: 10.1016/j.surfcoat.2019.05.042.
  6. Pakdel, H., & Mohammadi, B. (2019). Stiffness degradation of composite laminates due to matrix cracking and induced delamination during tension-tension fatigue. Engineering Fracture Mechanics, 216, 106489. DOI: 10.1016/j.engfracmech.2019.106489.
  7. Shojaee, T., Mohammadi, B., Madoliat, R., & Salimi-Majd, D. (2019). Development of a finite strip method for efficient prediction of buckling and post-buckling in composite laminates containing a cutout with/without stiffener. Composite Structures, 210, 538-552. DOI: 10.1016/j.compstruct.2018.11.007
  8. Mohammadi, B., & Khoddami, A. (2019). Representative volume element-based simulation of multiple solid particles erosion of a compressor blade considering temperature effect. Proceedings of the Institution of Mechanical Engineers, Part J: Journal of Engineering Tribology, 1350650119884825. DOI: 10.1177/1350650119884825
  9. Fazlali, B., & Mohammadi, B. (2019). A microscale energy-based fatigue damage model for unidirectional composites under multiaxial loading at different stress ratios. Engineering Fracture Mechanics, 205, 120-135. DOI: 10.1016/j.engfracmech.2018.11.024
  10. Shojaee, T., Mohammadi, B., & Madoliat, R. (2019). Experimental and numerical investigation of stiffener effects on buckling strength of composite laminates with circular cutout. Journal of Composite Materials, 0021998319874101. DOI: 10.1177/0021998319874101
  11. Mahmoudi, A., Mohammadi, B., & Hosseini‐Toudeshky, H. (2019). Damage behaviour of laminated composites during fatigue loading. Fatigue & Fracture of Engineering Materials & Structures. DOI: 10.1111/ffe.13152
  12. Noroozi, M., Mohammadi, B., Radiman, S., & Zakaria, A. (2019). Photothermal Effect of Modulating Laser Irradiation on the Thermal Diffusivity of Al 2 O 3 Nanofluids. Nanoscale research letters, 14(1), 1-10. DOI: 10.1186/s11671-019-2869-2
  13. Pakdel, H., & Mohammadi, B. (2018). Characteristic damage state of symmetric laminates subject to uniaxial monotonic-fatigue loading. Engineering Fracture Mechanics, 199, 86-100.  DOI: 10.1186/s11671-019-2869-2
  14. Shojaee, T., Mohammadi, B., Madoliat, R., & Salimi-Majd, D. (2019). Development of a finite strip method for efficient prediction of buckling and post-buckling in composite laminates containing a cutout with/without stiffener. Composite Structures, 210, 538-552. DOI: 10.1186/s11671-019-2869-2.
  15. Pakdel, H., & Mohammadi, B. (2018). Prediction of outer-ply matrix crack density at saturation in laminates under static and fatigue loading. International Journal of Solids and Structures, 139, 43-54. DOI: 10.1016/j.ijsolstr.2018.01.021
  16. Mohammadi, B., & Pakdel, H. (2018). Fatigue driven matrix crack propagation in laminated composites. Materials & Design, 146, 108-115. DOI: 10.1016/j.matdes.2018.02.067.
  17. Mohammadi, B., Abbaszadeh, M., & Keshmiri, A. (2018). Variational approach development in analysis of matrix cracking and induced delamination of cross-ply composite laminates subjected to in-plane shear loading. Mechanics of Advanced Materials and Structures, 25(6), 481-499. DOI: 10.1080/15376494.2017.1285456.
  18. Pakdel, H., & Mohammadi, B. (2018). Progressive matrix cracking master curves of mid and outer off-axis plies in CFRP laminates. Composite Structures, 188, 497-502. DOI: 10.1016/j.compstruct.2018.01.034.
  19. Mohammadi, B., & Pakdel, H. (2018). Experimental and variational-based analytical investigation of multiple cracked angle-ply laminates. Engineering Fracture Mechanics, 190, 198-212. DOI: 10.1016/j.engfracmech.2017.12.003
  20. Mohammadi, B., & Fazlali, B. (2018). Off-axis fatigue behaviour of unidirectional laminates based on a microscale fatigue damage model under different stress ratios. International Journal of Fatigue, 106, 11-23. DOI: 10.1016/j.ijfatigue.2017.09.004.
  21. Pakdel, H., & Mohammadi, B. (2017). Experimental observation and energy based analytical investigation of matrix cracking distribution pattern in angle-ply laminates. Theoretical and Applied Fracture Mechanics, 92, 146-154. DOI: 10.1016/j.tafmec.2017.06.007.
  22. Mohammadi, B., Rohanifar, M., Salimi-Majd, D., & Farrokhabadi, A. (2017). Micromechanical prediction of damage due to transverse ply cracking under fatigue loading in composite laminates. Journal of Reinforced Plastics and Composites, 36(5), 377-395. DOI: 10.1177/0731684416676635.
  23. Mohammadi, B., Fazlali, B., & Salimi-Majd, D. (2017). Development of a continuum damage model for fatigue life prediction of laminated composites. Composites Part A: Applied Science and Manufacturing, 93, 163-176. DOI: 10.1016/j.compositesa.2016.11.021.
  24. Jamali, M., Shojaee, T., Kolahchi, R., & Mohammadi, B. (2016). Buckling analysis of nanocomposite cut out plate using domain decomposition method and orthogonal polynomials. Steel and Composite Structures, 22(3), 691-712. DOI: 10.12989/scs.2016.22.3.691.
  25. 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.
  26. Jamali, M., Shojaee, T., & Mohammadi, B. (2016). Uniaxial buckling analysis comparison of nanoplate and nanocomposite plate with central square cut out using domain decomposition method. Journal of Applied and Computational Mechanics, 2(4), 230-242. DOI: 10.22055/jacm.2016.12543.
  27. Mohammadi, B., & Shahabi, F. (2016). 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, 152, 88-104. DOI: 10.22055/jacm.2016.12543.
  28. Mohammadi, B., Olia, H., & Hosseini-Toudeshky, H. (2015). Intra and damage analysis of laminated composites using coupled continuum damage mechanics with cohesive interface layer. Composite Structures, 120, 519-530. DOI: 10.1016/j.compstruct.2014.10.004.
  29. 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.
  30. 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.

  31. 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.

  32. 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

  33. M. Haghbeigi, E. Badrikouhi, B. Mohammadi: Dynamic Analysis and Simulation of an Aircraft Landing Gear System.

  34. 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.

  35. 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.

  36. 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.

  37. 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.

  38. 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.

  39. 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.

  40. 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.

  41. 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.

  42. 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.

  43. 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.

  44. 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.

  45. 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.

  46. 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.

  47. 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.

  48. 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.

  49. 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.

  50. 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.

  51. 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.

  52. 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.

  53. 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.

  54. 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.

  55. 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.

  56. 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.

  57. 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.

  58. 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.

  59. 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.

  60. 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.

  61. 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.

  62. 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.

  63. 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.

  64. 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.

  65. 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.

  66. 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.

  67. 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.

  68. 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.

  69. 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.

  70. 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.

  71. 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.

  72. 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.

  73. 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.

  74. 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.

  75. 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.

  76. 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.

  77. 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.

  78. 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.

  79. 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.

  80. 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.

  81. 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.

  82. 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.

  83. 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.

  84. 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.

  85. 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.

  86. 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.

  87. 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.

  88. 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.

  89. 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.

  90. 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.

  91. 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

  92. 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.

  93. 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.

  94. 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)

پروژه اول درس مکانیک خرابی در مواد کامپوزیت

پروژه نهایی درس مکانیک خرابی در مواد کامپوزیت سال تحصیلی 94-95

پروژه نهایی درس مکانیک خرابی در مواد کامپوزیت سال تحصیلی 95-96

محتویات دروس ارائه شده 

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