An experimental study on aerodynamics of NACA2415 aerofoil at low Re numbers
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 …
by varying angle of attack from− 12° to 20° at low Reynolds number flight regimes (0.5× 105 …
[图书][B] Low Reynolds Number: Aerodynamics and Transition
MS Genç - 2012 - books.google.com
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 …
transition from laminar to turbulence, unsteady low Reynolds number flows, experimental …
Interaction of tip vortex and laminar separation bubble over wings with different aspect ratios under low Reynolds numbers
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 …
considered experimentally at Reynolds numbers of 2.5× 104, 5× 104 and 7.5× 104. Studies …
Acoustic control of flow over NACA 2415 aerofoil at low Reynolds numbers
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 …
laminar separation bubble (LSB) and stall were explained. Then a literature review on the …
[HTML][HTML] Numerical study of separation on the trailing edge of a symmetrical airfoil at a low Reynolds number
J Lei, F Guo, C Huang - Chinese Journal of Aeronautics, 2013 - Elsevier
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 …
number. Finite volume method is adopted to solve the unsteady Reynolds-averaged Navier …
Numerical simulation of flow through an axisymmetric two-dimensional plane diffuser based on a new two-fluid turbulence model
Z Malikov, A Mirzoev, M Madaliev… - 2021 International …, 2021 - ieeexplore.ieee.org
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 …
axisymmetric two-dimensional diffusers. The calculations were performed on the basis of …
Aerodynamic behavior and flow visualization on canonical NACA airfoils at low Reynolds number
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 …
at Reynolds number values less than 5× 10 5 based on chord length. However, there are …
Improving the aerodynamic performance of wig aircraft with a micro-vortex generator (mvg) in low-speed condition
Z Methal, ASA Talib, MSA Bakar, MRA Rahman… - Aerospace, 2023 - mdpi.com
This present study investigated the potential of passive flow control to reduce induced drag
by using a micro-vortex generator (MVG) at a backward-facing step (BFS) location. A wing-in …
by using a micro-vortex generator (MVG) at a backward-facing step (BFS) location. A wing-in …
Phase portrait analysis of laminar separation bubble and ground clearance interaction at critical (low) Reynolds number flow
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 …
performance of Micro Aerial Vehicles (MAVs). Because of the being small in size, these birds …
Comparison of Aerodynamics Characteristics of NACA 0015 & NACA 4415
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 …
aerodynamic shape. Both of the shapes are extensively used for various kind of applications …