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Addresses: School of Mechanical Engineering, Iran University of Science & Technology, Narmak, Tehran, Iran

Zip Code: 16846-13114

Mail Box: 16765-163

Tel : +98(21) 77491228-29

Fax : +98(21) 77240488

Email: meresearch@iust.ac.ir

:: Mohammadi, Bijan ::

Full Name: Dr. Mohammadi, Bijan

 Position: Associate Professor

 Phone: 98-21-77240540-50 Ex:8967

 Phone: 98-21-77240208

 Fax: 98-21-77240488

 Email: Bijan_Mohammadi @ iust.ac.ir

 Webpages: http://webpages.iust.ac.ir/Bijan_Mohammadi



 Address: Iran University of Science & Tech., Tehran, IRAN


   University Degrees                            

  Fields of interest

  •   Local Continuum Damage Mechanics
  •   Non-local Continuum Damage Mechanics
  •   Damage Analysis in Laminated Composites
  •   Computational Fracture Mechanics
  •   Aerospace Structural Design
  •   Aerospace Structural Instability
  •   Aerospace Structural Analysis

  Research Projects

  •   “Developing a FEM based crack growth software”, HESA Co., 2010.
  •   “Remaining life assessment of aircraft structure”, HESA Co., 2010.

  Software Development 

       1-  FLAi : Fatigue Life Assessment software for estimation of fatigue life of metallic structures

       2- PALS : Professional Aircraft Loading software for estimation of critical loadings of transport

                     aircrafts under several flight conditions.

       3- Comp-Heat : One-dimensional thermal analysis in composite laminates

                              under several boundary condition (convection, conduction and radiation)

       4- NACA Inlet Design 5- Engine – VPCS propeller coupling performance

  Journal Papers

  1. B. Mohammadi, B Fazlali, Off-axis fatigue behaviour of unidirectional laminates based on a microscale fatigue damage model under different stress ratios,  Int. Journal of Fatigue, 106, 11-23, 2018.
  2. D Rahmatabadi, R Hashemi, B Mohammadi, T Shojaee, Experimental evaluation of the plane stress fracture toughness for ultra-fine grained aluminum specimens prepared by accumulative roll bonding process,  Materials Science and Engineering: A 708, 301-310, 2017.
  3. H Pakdel, B Mohammadi, Experimental observation and energy based analytical investigation of matrix cracking distribution pattern in angle-ply laminates, Theoretical and Applied Fracture Mechanics, In Press.  2017.
  4. B. Mohammadi, M Abbaszadeh, A Keshmiri, 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, 1-19, In Press, 2017.
  5. B. Mohammadi, B Fazlali, D Salimi-Majd, Development of a continuum damage model for fatigue life prediction of laminated composites, Composites Part A,  93, 163-176, 2017.
  6. 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 24 (2), 131-141, 2017.
  7. B. Mohammadi, M. Rohanifar, D Salimi-Majd, A Farrokhabadi, Micromechanical prediction of damage due to transverse ply cracking under fatigue loading in composite laminates,  Journal of Reinforced Plastics and Composites,   2017.
  8. H Darban, B. Mohammadi, F Djavanroodi, Effect of equal channel angular pressing on fracture toughness of Al-7075, Engineering Failure Analysis 65, 1-10, 2016.
  9. M Nikbakht, HH Toudeshky, B. Mohammadi, Experimental validation of an empirical nonlinear shear failure model for laminated composite materials, J. of Composite Materials, In Press, 2016.
  10. S GHIASVAND, B. MOHAMMADI, Mixed mode fatigue crack growth analysis of cracked aluminium panel repaired with composite patches using extended finite element method,  JOURNAL OF SCIENCE AND TECHNOLOGY OF COMPOSITES (JSTC) 3 (4), 321-332, 2017.
  11. B MOHAMMADI, S. Kamkar, A FARROKHABADI, Matrix cracking and induced delamination in symmetrically laminated composites subjected to static loading by using multi scale damage mechanics, JOURNAL OF SCIENCE AND TECHNOLOGY OF COMPOSITES (JSTC) 4 (1), 9-24, 2017.
  12. B. Mohammadi, M Helmi, MD SALIMI, Failure Prediction of Multidirectional Composite Laminates under Fatigue Loading using an Energy Based Damage Model,  AEROSPACE MECHANICS JOURNAL 13 (147), 95-108, 2017.
  13. M Jamali, T Shojaee, B Mohammadi, 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, 2016.
  14. M Jamali, T Shojaee, R Kolahchi, B. Mohammadi, Buckling analysis of nanocomposite cut out plate using domain decomposition method and orthogonal polynomials,  Steel & Composite Structures, An International Journal 22 (3), 691-712, 2016.
  15. M Nikbakht, H Hosseini Toudeshky, B. Mohammadi, Experimental study on the effect of interface fiber orientation and utilized delamination initiation techniques on fracture toughness of glass/epoxy composite laminates, , J. of Reinforced Plastics and Composites 35 (23), 1722-1733, 2016.
  16. 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
  17. 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

  18. 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

  19. 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

  20. 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

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

  22. 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

  23. 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

  24. 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

  25. 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

  26. G. Sadeghi, H. HosseiniToudeshky, 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

  27. 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

  28. 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

  29. 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

  30. 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

  31. 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

  32. 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

  33. 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

  34. 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

  35. 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

  36. 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

  37. 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

  38. 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

  39. 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

  40. 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. Proccedia Engineering

  41. 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

  42. 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

  43. 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

  44. 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

  45. 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

  46. 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

  47. 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

  48. 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

  49. 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

  50. 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

  51. 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

  52. 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

  53. 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

  54. 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

  55. 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

  56. 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

  57. 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

  58. 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

  59. 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

  60. 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

  61. 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

  62. 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

  63. 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

  64. 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

  65. 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

  66. 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

  67. 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

  68. 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

  69. 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

  70. 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

  71. 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

  72. 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

  73. 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

  74. 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

  75. 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

  76. 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

  77. 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

  78. 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

  79. 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

  80. 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

  81. 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

  82. 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.


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