Kh Md Faisal

We don’t have enough information about this author to calculate their statistics. If you think this is an error let us know.
Learn More
The growing interest in development of UAV has created a need for the comparative analysis of performance parameters of different aerofoils. Using this concept different characteristics of aerofoils are explored to design the wing of various UAV fulfilling various purposes. In this research work, the requirements of our desired UAV are established. These(More)
Aerodynamics of the rotary leading edge aircraft wing was experimented by the help of modified NACA-0010 airfoil. CFD simulation was done by converting the 2-D NACA-0010 airfoil to a 3-D aircraft wing. A cylinder was mounted at the leading edge of the modified aircraft wing and then it was allowed to rotate in anti-clockwise direction at a certain rpm. The(More)
  • 1