Mahdy Ahangar

Assistant Professor

Update: 2024-11-20

Mahdy Ahangar

New technologies and aerospace engineering /

Journal Paper

  1. "Wire-to-two-drop plasma thruster: Experimental and numerical investigation of electroaerodynamic jet flow for micro aerial vehicle propulsion"
    Mahdy Ahangar, NARGES ALEBRAHIM
    PHYSICS OF FLUIDS, Vol. 36, 2024
  2. "Augmented Interlaminar Fracture Toughness of Nanofibers-Interleaved Composite Laminates Via Plasma Treatment"
    Milad Saeedifar, Mahdy Ahangar
    JOURNAL OF MATERIALS SCIENCE, Vol. 59, pp.9291-9302, 2024
  3. "Experimental investigation on the performance of channel plasma thruster using tri-electrode DBD actuators under magnetic field"
    Mahdy Ahangar, Arefeh Hosseini
    SENSORS AND ACTUATORS A-PHYSICAL, Vol. 369, pp.115163-115175, 2024
  4. "The Effect of Plasma Treatment on the Mode II Interlaminar Fracture Toughness of Glass/Epoxy Laminates"
    Mahdy Ahangar, Milad Saeedifar
    THEORETICAL AND APPLIED FRACTURE MECHANICS, Vol. 127, pp.104093-104099, 2023
  5. "Theoretical study of electro-thermo-acoustic instability in a magneto-plasma-dynamic thruster"
    Mahdy Ahangar
    INTERNATIONAL JOURNAL OF THERMAL SCIENCES, Vol. 134, pp.410-420, 2018
  6. "Analytical investigation of anode heat flux in a magnetoplasmadynamic thruster"
    Mahdy Ahangar
    APPLIED THERMAL ENGINEERING, Vol. 118, pp.73-81, 2017
  7. "Numerical Investigation of Plasma Behavior and Anode Sheath in a Magnetoplasmadynamic Thruster"
    Mahdy Ahangar, Reza Ebrahimi, Mehrzad Shams
    JOURNAL OF PROPULSION AND POWER, Vol. 32, pp.420-430, 2016
  8. "Numerical simulation of non-equilibrium plasma flow in a cylindrical MPD thruster using a high-order flux-difference splitting method"
    Mahdy Ahangar, Reza Ebrahimi, Mehrzad Shams
    ACTA ASTRONAUTICA, Vol. 103, pp.129-141, 2014
  9. "Experimental performance characterization of a dielectric barrier discharge plasma thruster for propulsion applications"
    Mahdy Ahangar, Sarvgol Ahmadian
    مهندسی مکانیک دانشگاه تبریز, Vol. 52, pp.271-280, 2022
  10. "Experimental Study of the Performance Parameters of a Plasma Thruster Using Dielectric Barrier Discharge with the Magnetic Field"
    Mahdy Ahangar, Arefeh Hosseini
    مهندسی مکانیک مدرس, Vol. 22, pp.394-406, 2022
  11. "Numerical Modeling of plasma flow in an Electrohydrodynamic thruster with two-cathode electrode arrangement"
    Alireza Fathi, Mahdy Ahangar
    Journal of Space Science and Technology, Vol. 12, pp.1-10, 2019
  12. "Numerical Study of Plasma Impinging Jet Generated by Corona Discharge Regime"
    Alireza Fathi, Mahdy Ahangar
    مهندسی مکانیک دانشگاه تبریز, Vol. 49, pp.259-267, 2019
  13. "Numerical simulation of electrohydrodynamic flow produced by wire-to-cylinder in atmospheric condition"
    Alireza Fathi, Mahdy Ahangar
    مهندسی مکانیک مدرس, Vol. 18, pp.323-330, 2018
  14. "Numerical Phenomenology of Plasma Flow Near the Electrodes of a Magnetoplasmadynamic Thruster"
    Mahdy Ahangar
    مهندسی مکانیک دانشگاه تبریز, Vol. 47, pp.19-27, 2017
  15. "Investigation of Anode Electrothermal Process in a MPD Thruster"
    Mahdy Ahangar, Akram Sedigh
    مهندسی مکانیک مدرس, Vol. 17, pp.77-84, 2017
  16. "Development and Validation of an MHD Code for Study of Argon plasma Flow Characteristics in the PFSB Thruster"
    Mahdy Ahangar, Reza Ebrahimi, Mehrzad Shams
    مهندسی مکانیک دانشگاه تبریز, Vol. 46, pp.1-9, 2016
  17. "Numerical Simulation of Non-equilibrium Plasma Flow in a Magneto-plasmadynamic Thruster"
    Mahdy Ahangar, Ebrahimi Reza, Mehrzad Shams
    مکانیک سازه ها و شاره ها, Vol. 4, pp.89-101, 2014
  18. "The solution of MHD equations using a high order characteristics-splitting scheme for MPDT simulation"
    Mahdy Ahangar, Ebrahimi Reza, Mehrzad Shams
    مهندسی مکانیک مدرس, Vol. 13, pp.28-42, 2014
  19. "An Investigation on the Effect of Chemical Kinetics Mechanisms in the Modeling of Combustive Gaseous Oxidizer Flow on a Solid Fuel Surface"
    Mahdy Ahangar, Reza Ebrahimi
    علوم و فناوری فضایی, Vol. 3, pp.1-13, 2010
  20. "Numerical Modeling of HTPB/O2 Combustion Process in a Hybrid Rocket Motor to Determine Solid Fuel Surface Regression Rate"
    Mahdy Ahangar, Reza Ebrahimi, Akbar Ghafourian
    سوخت و احتراق, Vol. 2, pp.1-39, 2009