All Stories

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

    Article • Propulsion and Power Research, July 2020, Elsevier

    Dr Mohamed SELLAM

  2. 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

  3. 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

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

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

    Dr Mohamed SELLAM

  5. 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

  6. 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

  7. Design and performance evaluation of a dual bell nozzle

    Article • Acta Astronautica, January 2017, Elsevier

    Dr Mohamed SELLAM

  8. 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

  9. 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

  10. 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

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

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

    Dr Mohamed SELLAM

  12. Design and performances of the dual-bell nozzle

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

    Dr Mohamed SELLAM

  13. 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

  14. Numerical Study of Transonic Flows Using Various Turbulence Models

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

    Dr Mohamed SELLAM

  15. 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

  16. 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

  17. Aeroelastic stability analysis of flexible overexpanded rocket nozzle

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

    Dr Mohamed SELLAM

  18. 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

  19. 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

  20. Numerical investigation of overexpanded nozzle flows

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

    Dr Mohamed SELLAM

  21. 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

  22. 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

  23. 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

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

    Article • January 2012, Springer Science + Business Media

    Dr Mohamed SELLAM

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

    Article • January 2012, Springer Science + Business Media

    Dr Mohamed SELLAM

  26. 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

  27. Shock Waves

    Article • January 2009, Springer Science + Business Media

    Dr Mohamed SELLAM