Evaluation of wing performance for NACA 4415 using subparametric finite element transforms
The goal of the current research is to improve the lift performance of an aerodynamic device
for commercial application by performing accurate aerodynamic computations and flow …
for commercial application by performing accurate aerodynamic computations and flow …
Vortex lattice simulations of attached and separated flows around flap** wings
Flap** flight is an increasingly popular area of research, with applications to micro-
unmanned air vehicles and animal flight biomechanics. Fast, but accurate methods for …
unmanned air vehicles and animal flight biomechanics. Fast, but accurate methods for …
Aerodynamic Performance of Symmetric and Cambered Airfoils at Low Reynolds Numbers
A Cruz, A Rodriguez… - Fluids …, 2022 - asmedigitalcollection.asme.org
The aerodynamics of airfoils has been extensively studied at high Reynolds numbers, where
approximations of variables such as drag, and lift can easily be obtained based on …
approximations of variables such as drag, and lift can easily be obtained based on …
[PDF][PDF] Numerical validation of NACA 0009 airfoil in ultra-low reynolds number flows
A Seeni, P Rajendran - Int. Rev. Aerosp. Eng, 2019 - researchgate.net
Validation of the sectional airfoil performance is necessary to test a propeller. This study
presents a numerical validation of the computational fluid dynamics (CFD) method for testing …
presents a numerical validation of the computational fluid dynamics (CFD) method for testing …
Numerical investigation and parametric study of NACA 0009 airfoil with bumps inspired by mako-shark skin denticles
RM Arjanki, M Pasandidehfard… - Proceedings of the …, 2024 - journals.sagepub.com
In the current research, a numerical study of 53 airfoils inspired by the surface scales of the
mako-shark skin based on NACA0009 airfoil has been performed. The airflow simulations …
mako-shark skin based on NACA0009 airfoil has been performed. The airflow simulations …
Effect of grooves on aerodynamic performance of a low reynolds number propeller
AS Seeni - 2020 - erepo.usm.my
UAVs in the future will be designed for next-generation applications such as product delivery
from source to end-user. These UAVs weigh in the range of 1 to 10 kg and are powered by …
from source to end-user. These UAVs weigh in the range of 1 to 10 kg and are powered by …
[PDF][PDF] Sharp Leading-Edge Symmetric Airfoils In Low Reynolds Number Flow
J Rud - 2022 - scholarworks.calstate.edu
Acknowledgements I would like to thank Dr. Hamid Johari for his guidance and support
throughout the research process, answering questions, and providing references to …
throughout the research process, answering questions, and providing references to …
[PDF][PDF] Simulating Airfoils at Ultra-Low Reynolds Numbers using Panel Methods
E Morenoa, A Rodriguezb, J Herreraa, R Adansib… - researchgate.net
Simulating Airfoils at Ultra-Low Reynolds Numbers using Panel Methods Page 1 Simulating
Airfoils at Ultra-Low Reynolds Numbers using Panel Methods E. Morenoa2, A. Rodriguezb+1 …
Airfoils at Ultra-Low Reynolds Numbers using Panel Methods E. Morenoa2, A. Rodriguezb+1 …
[PDF][PDF] Enhancement of Airfoil Performance by Rotating Cylinder
MS Kadhim, DA Hamzah - 2021 - iasj.net
This study used a NACA 6409 smooth wing section. Its performance is compared to an
enhanced design incorporating a revolving cylinder on the upper airfoil surface. The …
enhanced design incorporating a revolving cylinder on the upper airfoil surface. The …