Micro air vehicle research has exponentially expanded since the first articles began to be
published in the late 1990s. This article presents a comprehensive bibliometric review of …

Purpose One of the best methods to improve wind turbine aerodynamic performance is
modification of the blade's airfoil. The purpose of this paper is to investigate the effects of …

This study investigates the effects of positive horizontal acceleration of the freestream
velocity on a pitch‐oscillating VR‐12 airfoil using computational fluid dynamics. The shear …

Purpose–The main aim of the present work is to examine the effects of trailing edge strip
(TES) on the wake region of a plunging airfoil that oscillates prior and beyond the static stall …

The unsteady flow field in the wake of an NACA 23012 pitching airfoil was investigated by
means of triple hot‐wire probe measurements. Wind tunnel tests were carried out both in the …

Boundary layer and wake behaviors are strongly affected by airfoil motion. Moreover,
parameters like body oscillation frequency, oscillation type, Mach number, and angle of …

Aerodynamic performance and stability parameters of high wing piston engine aircraft were
evaluated using Computational Fluid Dynamics and validated against wind tunnel test and …

Experimental investigations were carried out to study the wake characteristics of a pitching
supercritical airfoil at Mach number of 0.6. Flow field inside the wake was measured by a hot …

Experimental investigations were carried out to study the wake profile of a supercritical airfoil
at Mach numbers of 0.4 and 0.6 in a pitching motion. Both static and dynamic tests were …

Experimental measurements were conducted on a plunging Eppler 361 Gurney flapped
airfoil to study wake structure and dynamic stall phenomenon in the wake. The heights of …