Since its invention by a race car driver Dan Gurney in 1960s, the Gurney flap has been used
to enhance the aerodynamics performance of subsonic and supercritical airfoils, high-lift …

A Gurney flap (GF) placed at pressure side of the trailing edge of an airfoil and
perpendicular to the chord line enhances lift in aircraft wings, helicopter rotors, and wind …

The aerodynamic effects of the application of Gurney flaps of different heights and chordwise
locations to five airfoils have been investigated in the Pennsylvania State University low …

A two-dimensional steady Reynolds-averaged Navier–Stokes (RANS) equation was solved
to investigate the effects of a Gurney flap on SFYT15thick airfoil aerodynamic performance …

The impact of Gurney flaps (GF), of different heights and perforations, on the aerodynamic
and wake characteristics of a NACA 0015 airfoil equipped with a trailing-edge flap (TEF) …

C= chord length CD= drag coefficient Cf= skin friction coefficient CL= lift coefficient CM=
quarter-chord pitching moment coefficient CP= pressure coefficient h= height of Gurney flap …

EVER-INCREASING application has driven a significant research effort to extend, refine,
and hone the available technological toolbox for unmanned aerial vehicles (UAVs). UAV …

Gurney flap is a miniature lift-enhancement device installed at the airfoil trailing edge and
has been successfully applied to fixed wing aircraft and low-speed horizontal wind turbines …

Since its inception in the early 1970s by Daniel Gurney, the Gurney flaps have proven to be
an effective means of enhancing the aerodynamic performance of an airfoil. Current …

Two-dimensional steady Reynolds-averaged Navier-Stokes (RANS) equations with
transition shear stress transport (SST) model were solved to investigate the effects of Gurney …