Publications

REFEREED JOURNAL PAPERS

  1. Mostafa El Sayed, MAG Contreras, N Stathopoulos, “Monitor Points Method for Loads Recovery in Static/Dynamic Aeroelasticity Analysis with Hybrid Airframe Representation”, SAE International Journal of Aerospace, Volume 6, Issue 2, pp. 399-407, DOI:10.4271/2013-01-2142. (2013).
  2. Mostafa El Sayed and Damiano Pasini, “Comprehensive Stiffness of Prestressed Lattice Materials”, Journal of Materials Science Research, Volume 1, Issue 2, pp. 87-109, DOI: 10.5539/jmsr.v1n2p87. (2012).
  3. Mostafa El Sayed and Damiano Pasini, “Analysis of the Elastostatic Specific Stiffness of 2D Stretching-Dominated Lattice Materials”, Journal of Mechanics of Materials, Volume 42, Issue 7, pp. 709-725, DOI:10.1016/j.mechmat.2010.05.003. (2010).
  4. Mostafa El Sayed and Damiano Pasini, “Multiscale Structural Design of Columns Made of Regular Octet-Truss Lattice Material”, International Journal of Solids and Structures, Volume 47, Issue 14, pp. 1764-1774, DOI:10.1016/j.ijsolstr.2010.03.003. (2010).
  5. Sridhar Chintapalli, Mostafa El Sayed, Ramin Sedaghati and Mohammed Abdo “The Development of a Preliminary Structural Design Optimization Method of an Aircraft Wing-Box Skin-Stringer Panels”, Journal of Aerospace Science and Technology, Volume 14, Issue 3, pp. 188-198, DOI:10.1016/j.ast.2009.12.007. (2009).
  6. Mostafa El Sayed, Ramin Sedaghati and Mohammed Abdo “Accurate Stick Model Development for Static Analysis of Complex Aircraft Wing-Box Structures”, AIAA Journal. Volume 47, Issue 9, pp. 2063-2075,  DOI: 10.2514/1.38447. (2009).
  7. Mostafa El Sayed and Damiano Pasini, “Mechanics of 2D Pin Jointed Lattice Structures”, AES Technical Reviews, Part B: International Journal of Advances in Mechanics and Applications of Industrial Materials, Volume 1, Issue 1, pp. 83 – 91. (2009).
  8. Mostafa El Sayed and H.A. Sherif, “Pre-Tensioned Layer Damping as a New Approach for Vibration Control of Elastic Structures”. Journal of Vibration and Acoustics (ASME), Volume 128, Issue 3, pp.338-346, doi:10.1115/1.2166855. (2006).

REFEREED CONFERENCE PAPERS

  1. Bacheva, Mostafa El Sayed, R.S.Trask, “The Skeleton of Euplectella Aspergillum as Foundation for the Development of Novel Composite Aerospace Structures”, 18th International Conference on composite materials, 21-26, Jeju, Korea, August 2011.
  2. Mostafa El Sayed and Damiano Pasini “Theoretical and Experimental Characterization of the 34.6 2D Lattice Material”. ASME 2010 International Design Engineering Technical Conferences & Computers and Information in Engineering Conference IDETC/CIEC, Montreal, Qc, Canada, August, 15-18, 2010.
  3. Mostafa El Sayed and Damiano Pasini “Structural Performance Analysis and Characterization of Novel 2D Stretching Dominated Infinite Lattice Materials”, ASME 2009 International Design Engineering Technical Conferences & Computers and Information in Engineering Conference IDETC/CIE, San Diego, California, USA, Aug 30- Sept 2, 2009.
  4. Mostafa El Sayed, Hébert Clément, and Damiano Pasini “Structural Analysis of Pin Jointed Lattice Structures”. Third International Conference on Advances and Trends in Engineering Materials and their Applications AES-TEMA 2009. McGill University, July 6-10 2009.
  5. Mostafa El Sayed and Damiano Pasini “Multi-Scale Model of the Effective Properties of the Octet-Truss Lattice Material”, AIAA Technical Conferences, Victoria, BC, Canada, September 10-12, 2008.
  6. Mostafa El Sayed, Ramin Sedaghati and Mohammed Abdo “New Approach for Generating Beam Models of Complex aircraft wing-box Structures Used for Static Aero-elasticity”, The Canadian Aeronautics and Space Institute Conference- CASI 2007 (Aero 07). April 2007.
  7. Mostafa El Sayed, H.A. Sherif and A.A. Omer, “New Approach for Vibration Control of a Cantilevered Beam”, 10th International Conference On Aerospace Sciences And Aviation Technology, Technical College, Cairo Egypt, pp. 527-537, 13-15 May, 2003.
  8. Mostafa El Sayed and H.A. Sherif “Smart Control of Base Excited Cantilevered Beam Using Active Constrained Layer Damping”, 10th International Conference On Applied Mechanics And Mechanical Engineering, Technical College, Cairo Egypt, pp. 154-160, 14-16 May, 2002.
  9. Mostafa El Sayed, Miguel Alejandro Gutierrez Contreras, Nicholas Stathopoulos, Bombardier Aerospace, “Monitor Points Method for Loads Recovery in Static/Dynamic Aeroelasticity Analysis with Hybrid Airframe Representation”, SAE 2013 Aero Tech Congress & Exhibition, September 2013.

TECHNICAL REPORTS (Selected)

  1. Mostafa El Sayed, 15.698.001.MS, “Bombardier Core Loads Field Service Support Reporting -CRJ1000 – SN19008”, Bombardier Aerospace, (2015), (Classified).
  2. Mostafa El Sayed,15.7000.018.MS, “Global 7000/8000, Loop 2, Ditching Loads”. Bombardier Aerospace, (2015). (Classified).
  3. Mostafa El Sayed,12.7000.038.K0A “G7000/G8000 Antenna Loads”, (2015). Bombardier Aerospace. (Classified).
  4. Mostafa El Sayed, LD.14.LJ200.021.MS “Learjet 85, Loop 2, Windmilling Fatigue Loads”. Bombardier Aerospace, (2014). (Classified).
  5. Mostafa El Sayed,14.LJ200.018.MS “Learjet 85, Loop 2, Windmilling Limit and Ultimate Load Envelopes”. Bombardier Aerospace. (Classified).
  6. Mostafa El Sayed, (2014). LD.14.LJ200.016.MS “Learjet 85, Loop 2, Windmilling Vibration Loads”. Bombardier Aerospace, (2014). (Classified).
  7. Mostafa El Sayed,14.7000.027.MSA “Global 7000/8000 AFT EGRESS Door 1G Max- Operational Retraction Loads”. Bombardier Aerospace, (2014). (Classified).
  8. Mostafa El Sayed,14.7000.016.MS “Preliminary Loads for Global 7000/8000 APU Door Side-skirt”. Bombardier Aerospace, (2014). (Classified).
  9. Mostafa El Sayed,13.7000.087.MS “Preliminary Loads for Global 7000/8000, Retracted/Deployed, FWD, EGRESS Door”. Bombardier Aerospace, (2013). (Classified).
  10. Mostafa El Sayed,13.7000.076.MS “Preliminary Limit Loads for the Global 7000/8000 Over Wing Emergency Exit Door”. Bombardier Aerospace, (2013). (Classified).
  11. Mostafa El Sayed,13.7000.082.MS “Global 7000 and Global 8000 Differential Pressure on Fuselage Tailcone”. Bombardier Aerospace, (2013). (Classified).
  12. Mostafa El Sayed,13.NCAP.046.MSA “CS100 Wing to Belly Fairing Consistent Aerodynamic Pressure Distribution at Critical Flight Conditions”. Bombardier Aerospace, (2013). (Classified).
  13. Mostafa El Sayed,13.7000.077.MS “Preliminary Limit Loads for the Global 7000/8000 Passengers Door”. Bombardier Aerospace, (2013). (Classified).
  14. Mostafa El Sayed,13.7000.046.MSA “Global 7000/8000 Loop1 Fatigue Loads Due to Windmilling Imbalance”. Bombardier Aerospace, (2013). (Classified).
  15. Mostafa El Sayed,13.7000.068.MS “Global 7000 & 8000 Gutter Aerodynamic Loads”. Bombardier Aerospace, (2013). (Classified).
  16. Mostafa El Sayed,13.7000.056.MS “Global 7000 & 8000 Louver Venting Aerodynamic Pressure Loads”. Bombardier Aerospace, (2013). (Classified).
  17. Mostafa El Sayed,13.7000.065.MS “Global 7000 & 8000 Cabin Windows Aerodynamic Pressure Loads versus Altitudes”. Bombardier Aerospace, (2013). (Classified).
  18. Mostafa El Sayed,13.7000.039.MSA “Global 7000 Discretized Windmilling Cases”. Bombardier Aerospace, (2013). (Classified).
  19. Mostafa El Sayed,13.7000.028.MS “Global 7000 and Global 8000 Accelerations due to Windmilling”. Bombardier Aerospace, (2013). (Classified).
  20. Mostafa El Sayed,13.7000.011.MS “G7000/G8000 Cockpit Smart Probe Loads”. Bombardier Aerospace, (2013). (Classified).
  21. Mostafa El Sayed, “Loads Monitoring as a New Approach for Loads Recovery Applications”. Bombardier Aerospace Manual, (2011). (Classified).
  22. Mostafa El Sayed, “The Bloch’s Theorem”. McGill University, Technical Report No. TR-MDOG-09-01, (2009).
  23. Mostafa El Sayed, Amandeep Sing and Ramin Sedaghati “Conceptual Design Optimization of an Aircraft Wing-Box Structure and Generating a High Fidelity Stick-Model”. Multidisciplinary Optimization Standardization Approach for Integration and Configurability (MOSAIC) Project, Sponsor’s Ref. No: CRIAQ 4.1-TASK 6. Technical Report, January 2007.
  24. Mostafa El Sayed and Ramin Sedaghati “Wing Rib Stress Analysis and Design Optimization”, Multidisciplinary Optimization Standardization Approach for Integration and Configurability (MOSAIC) Project, Sponsor’s Ref. No: CRIAQ 4.1-TASK 6. Technical Report, August 2006.
  25. Mostafa El Sayed, Amandeep Sing and Ramin Sedaghati “3D Finite Element Model of DLR-F6 aircraft Wing-Box Structure, Created in PATRAN and Analyzed in NASTRAN”. Multidisciplinary Optimization Standardization Approach for Integration and Configurability (MOSAIC) Project, Sponsor’s Ref. No: CRIAQ 4.1-TASK 6. Technical Report, September 2006.