A feature of laminar separated flows which occurs naturally, even at rather small Reynolds
numbers, is their instability. Thus, a mean flow pattern in a separated flow as well as its …

Shear layer development over a NACA 0018 airfoil at a chord Reynolds number of 100000
was investigated using a combination of flow visualization, velocity field mapping, surface …

To many a student, having to do a literature review is–simply put–a pain and something they
dread. Telling friends how I have started the work on this review before summer, I am often …

Transition and flow development in a separation bubble formed on an airfoil are studied
experimentally. The effects of tonal and broadband acoustic excitation are considered since …

A number of airfoils have been tested in the Pennsylvania State University low-speed low-
turbulence wind tunnel, and the results of these tests are compared with those predicted …

Laminar-turbulent boundary-layer transition is investigated on the suction side of Mach-
scaled helicopter rotor blades in climb and analyzed in view of the effect of rotational forces …

ABSTRACT Two‐dimensional (2D) and quasi‐three dimensional (3D), steady and unsteady,
viscous–inviscid interactive codes capable of predicting the aerodynamic behavior of wind …

Laminar-turbulent transition behaviour of a wind turbine blade section is investigated in this
study by means of field experiments and 3-D computational fluid dynamics (CFD) rotor …

The present report describes numerical investigation of two-dimensional unsteady airfoil
flows with application to aeroelastic stability. The report is divided in two parts. Part A …

In the present work, various data processing methods for laminar to turbulent transition
detection on airfoils are assessed based on experimental data. For this purpose, NACA 63 …