The bending response of laminated composite sandwich structures developed for aircraft
flaps is analyzed, in two parts. In the first part, the carbon fiber reinforced plastic (CFRP) and …

Since the invention of the aircraft, there has been a need for better surface design to
enhance performance. This thirst has driven many aerodynamicists to develop various types …

The aerodynamic characteristics of a NACA0012 wing geometry at low Reynold's numbers
and angle of attack ranging from 0º to 90º are investigated using numerical simulations and …

This study provides a view of the primary aerodynamic design of Hyperloop pod considering
the influence of tail shape and length on aerodynamic forces (drag and lift) and flow …

An analysis of 2D subsonic flow over an NACA 0015 airfoil with a 30% trailing edge flap at a
constant Reynolds number of 106 for various incidence angles and a range of flap …

In the present study, the effect of hinge position (H) has been numerically investigated to find
the appropriate position for improving the aerodynamic performance of the NACA 0012 …

The lift and drag coefficient plots for any airfoil provides a means for measuring its
aerodynamic characteristics. These are very useful in deciding if a particular airfoil is …

The unmanned aerial vehicle (UAV) is becoming popular from last two decades and it has
been utilizing in enormous applications such as aerial monitoring, military purposes, rescue …

Recently, the exceptional manoeuvrability and stealth characteristics of manta-like fish have
sparked significant interest in the development of bionic underwater vehicles. This study …

Selection of an appropriate and efficient turbulence models is important for fast and accurate
computation in fluid dynamics. In order to investigate the computational efficiency of …