All Stories

  1. Experimental and numerical investigation of transverse secondary injection in dual-bell nozzles for enhanced operating mode switch control

    Article • Acta Astronautica, November 2025, Elsevier

    Dr Mohamed SELLAM

  2. CFD investigation of supersonic two parallel expansions nozzles

    Article • Advances in Space Research, January 2025, Elsevier

    Dr Mohamed SELLAM

  3. Advanced piezoelectric fluid energy harvesters by monolithic fluid–structure–piezoelectric coupling: A full-scale finite element model

    Article • Physics of Fluids, November 2024, American Institute of Physics

    Runze ZHANG, Dr Mohamed SELLAM

  4. Bandgap analysis of periodic composite plates considering fluid–structure coupling

    Article • Journal of Sound and Vibration, July 2024, Elsevier

    Dr Mohamed SELLAM

  5. Parametrical Investigation of Transverse Injection in a Dual-Bell Nozzle During Altitude-Varying Conditions

    Article • Journal of Propulsion and Power, November 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mohamed SELLAM

  6. Experimental investigation of forced flow regime transition in a dual bell nozzle by secondary fluidic injection

    Article • International Journal of Heat and Fluid Flow, June 2021, Elsevier

    Dr Mohamed SELLAM

  7. Controlled flow regime transition in a dual bell nozzle by secondary radial injection

    Article • Experiments in Fluids, November 2020, Springer Science + Business Media

    Dr Mohamed SELLAM

  8. Effect of reacting gas on the fluidic thrust vectoring of an axisymmetric nozzle

    Article • Propulsion and Power Research, July 2020, Elsevier

    Dr Mohamed SELLAM

  9. Effect of Chemical Reactions on the Fluidic Thrust Vectoring of a Plane Nozzle

    Article • Arabian Journal for Science and Engineering, January 2020, Springer Science + Business Media

    Dr Mohamed SELLAM

  10. Performance improvement of supersonic nozzles design using a high-temperature model

    Article • Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, February 2019, SAGE Publications

    zebbiche toufik, Dr Mohamed SELLAM

  11. Numerical study of a nonequilibrium H2−O2 rocket nozzle flow

    Article • International Journal of Hydrogen Energy, February 2019, Elsevier

    Dr Mohamed SELLAM

  12. Effect of chemical reactions on the fluidic thrust vectoring of an axisymmetric nozzle

    Article • International Journal of Aviation Aeronautics and Aerospace, January 2019, Embry-Riddle Aeronautical University/Hunt Library

    Dr Mohamed SELLAM

  13. Assessment of transition regimes in a dual-bell nozzle and possibility of active fluidic control

    Article • Aerospace Science and Technology, November 2018, Elsevier

    Dr Mohamed SELLAM

  14. Design and performance evaluation of a dual bell nozzle

    Article • Acta Astronautica, January 2017, Elsevier

    Dr Mohamed SELLAM

  15. Adaptation of the Transpiration Method to Simulate the Fluid–Structure Interaction Phenomena for a Flexible Overexpanded Rocket Nozzle

    Article • January 2017, Springer Science + Business Media

    Dr Mohamed SELLAM

  16. New Modified Pekkari Model to Analyse the Aeroelastic Stability Behaviour for a Flexible Overexpanded Rocket Nozzle

    Article • January 2017, Springer Science + Business Media

    Dr Mohamed SELLAM

  17. Secondary Injectant Gas Thermodynamic Properties Effects on Fluidic Thrust Vectoring Performances of a Supersonic Nozzle

    Article • January 2017, Springer Science + Business Media

    Dr Mohamed SELLAM

  18. Erratum to: Aeroelastic stability analysis of flexible overexpanded rocket nozzle

    Article • Shock Waves, July 2016, Springer Science + Business Media

    Dr Mohamed SELLAM

  19. Design and performances of the dual-bell nozzle

    Article • March 2016, Institute of Electrical & Electronics Engineers (IEEE)

    Dr Mohamed SELLAM

  20. Experimental–Numerical Parametric Investigation of a Rocket Nozzle Secondary Injection Thrust Vectoring

    Article • Journal of Propulsion and Power, January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mohamed SELLAM

  21. Numerical Study of Transonic Flows Using Various Turbulence Models

    Article • International Review of Aerospace Engineering (IREASE), December 2015, Praise Worthy Prize

    Dr Mohamed SELLAM

  22. Aeroelastic stability analysis of a flexible over-expanded rocket nozzle using numerical coupling by the method of transpiration

    Article • Journal of Fluids and Structures, July 2015, Elsevier

    Dr Mohamed SELLAM

  23. Assessment of gas thermodynamic characteristics on fluidic thrust vectoring performance: Analytical, experimental and numerical study

    Article • International Journal of Heat and Fluid Flow, June 2015, Elsevier

    Dr Mohamed SELLAM

  24. Aeroelastic stability analysis of flexible overexpanded rocket nozzle

    Article • Shock Waves, May 2015, Springer Science + Business Media

    Dr Mohamed SELLAM

  25. Numerical Simulation of Reactive Flows in Overexpanded Supersonic Nozzle with Film Cooling

    Article • International Journal of Aerospace Engineering, January 2015, Hindawi Publishing Corporation

    Dr Mohamed SELLAM

  26. Thrust shock vector control of an axisymmetric conical supersonic nozzle via secondary transverse gas injection

    Article • Shock Waves, October 2013, Springer Science + Business Media

    Dr Mohamed SELLAM

  27. Numerical investigation of overexpanded nozzle flows

    Article • Shock Waves, July 2013, Springer Science + Business Media

    Dr Mohamed SELLAM

  28. Visualization by discharge illumination technique and modification by plasma actuator of rarefied Mach 2 airflow around a cylinder

    Article • Measurement Science and Technology, May 2013, Institute of Physics Publishing

    Dr Mohamed SELLAM

  29. Thrust vectoring effects of a transverse gas injection into a supersonic cross flow of an axisymmetric convergent-divergent nozzle

    Article • January 2013, EDP Sciences

    Dr Mohamed SELLAM

  30. Effects of the Inlet Gases Thermodynamic Properties on a Fluidically Thrust Vectorized Supersonic Nozzle

    Article • September 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mohamed SELLAM

  31. Experimental and Numerical Study of Thrust-Vectoring Effects by Transverse Gas Injection into a Propulsive Axisymmetric C-D Nozzle

    Article • July 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Mohamed SELLAM

  32. Numerical Investigation of Over-Expanded Nozzle Flows: Influence of Internal Shock Waves

    Article • January 2012, Springer Science + Business Media

    Dr Mohamed SELLAM

  33. Thrust Shock Vector Control of an Axisymmetric C-D Nozzle via Transverse Gas Injection

    Article • January 2012, Springer Science + Business Media

    Dr Mohamed SELLAM

  34. Fluidic thrust vectoring of an axisymmetrical nozzle: an analytical model

    Article • International Journal of Aerodynamics, January 2012, Inderscience Publishers

    Dr Mohamed SELLAM

  35. Numerical Study of Heat Transfer Around the Small Scale Airfoil Using Various Turbulence Models

    Article • Numerical Heat Transfer Part A Applications, December 2009, Taylor & Francis

    Dr Mohamed SELLAM

  36. Shock Waves

    Article • January 2009, Springer Science + Business Media

    Dr Mohamed SELLAM