Employee Details


Faculty of Mechanical Engineering


B.Sc. in Aeronautical Engineering,
Military Institute of Science and Technology (MIST),
Bangladesh University of Professionals (BUP), Mirpur, Dhaka-1216, Bangladesh.



Lecturer, Department of Aeronautical Engineering.

Military Institute of Science and Technology (MIST),

Bangladesh University of Professionals (BUP).

Theory Courses Taken                                                 Lab Courses Taken
1. Space Engineering                                                      1. Wind Tunnel Sessional
2. Aircraft Stability & Control                                            2. CFD Sessional
3.Computational Structural Analysis                                3. Material Science Sessional
4. Machine Design

4. Thermodynamics Sessional



Chancellor’s Gold Medal of Bangladesh University of Professionals 

Osmany Memorial Gold Medal

Best Project 2016 Award fromAeronautical Engineering Dept., MIST(Team Member)

MIST Commandant’s List (2013,2014,2015,2016)



Comparative Assessment of Turbulence Model in PredictingAirflow over a NACA 0010 Airfoil.

Shoyon Panday, Nafiz Ahmed Khan, Md Rasel, Kh. Md. Faisal and Md.Abdus Salam.

7th BSME International Conference on Thermal Engineering

AIP Conf. Proc. 1851, 020045-1–020045-6; doi: 10.1063/1.4984674

Published by the American Institute of Physics.


Design of a Small Unmanned Mother Ship

Shoyon Panday, Nafiz Ahmed Khan, MobasseraBelalTiasha, Kh. Md. Faisal and Md. Abdus Salam.

Proceedings of 12th Global Engineering, Science and Technology Conference.

23 – 24 December 2016, BIAM Foundation, 63 New Eskaton, Dhaka, Bangladesh.

ISBN: 978-1-925488-25-8


Detail Design of Empennage of an Unmanned Aerial Vehicle

Md. Samad Sarker, Shoyon Panday, Md Rasel, Md. Abdus Salam, Kh. Md. Faisal,Tanzimul Farabi.

International Conference on Mechanical Engineering and Applied Science (ICMEAS 2017), 22-23 February 2017, Dhaka, Bangladesh.



Comparative Assessment of Various Turbulence Models and Improved Performanceof NACA0010 Airfoil with MSBLC (Moving Surface Boundary Layer Control) .

A comparative study was carried out to show the effect of turbulence models of ANSYS on flow analysis over NACA 0010 airfoil. The effect of moving surface boundary layer control was also observed by mounting a cylinder at the leading edge of the airfoil. (Undergraduate Thesis)



  • Design and fabrication of a Mother Ship with Small Aerial Vehicles: FUTURE FLIGHT DESIGN 2015,Istanbul, Turkey. (Team Leader)
  • Design and demonstration of a Manufacturing UAV and a Production UAV for specific 2015-2016 mission profile of AIAA Student Design/Build/Fly (DBF) Competition, Wichita, KS, USA. (Selected in the Aircraft Design Phase)(Design Group Head)
  • Design and fabrication of an Air to Air Target Drone. (On Going) (Member of Design Group)
  • 1st National Aero Design Competition arranged by MIST. (Team Leader)