This study is a detailed experimental investigation on aerodynamics of a NACA2415 aerofoil
by varying angle of attack from− 12° to 20° at low Reynolds number flight regimes (0.5× 105 …

Abstract We study the Laminar Separation Bubble (LSB) which develops on the suction side
of a NACA 0015 hydrofoil by means of a Temperature-Sensitive Paint (TSP), at a Reynolds …

This book reports the latest development and trends in the low Re number aerodynamics,
transition from laminar to turbulence, unsteady low Reynolds number flows, experimental …

In present study, aerodynamics of a NACA4412 wings with aspect ratio of 1 and 3 was
considered experimentally at Reynolds numbers of 2.5× 104, 5× 104 and 7.5× 104. Studies …

Within the concept of this study, first low Reynolds number flow phenomena, including
laminar separation bubble (LSB) and stall were explained. Then a literature review on the …

This study focuses on the trailing-edge separation of a symmetrical airfoil at a low Reynolds
number. Finite volume method is adopted to solve the unsteady Reynolds-averaged Navier …

NACA 0015 and NACA 4415 aerofoil are most common four digits and broadly used
aerodynamic shape. Both of the shapes are extensively used for various kind of applications …

The paper presents the results of a numerical study of the structure of flow through
axisymmetric two-dimensional diffusers. The calculations were performed on the basis of …

Some unmanned aerial vehicles, micro-air vehicles, and small-scale wind turbines operate
at Reynolds number values less than 5× 10 5 based on chord length. However, there are …

Inspiring from nature, flying near the ground surface might increase the aerodynamic
performance of Micro Aerial Vehicles (MAVs). Because of the being small in size, these birds …