Systematic reduced order model development of a pitching NACA0012 airfoil
J Mohrfeld Halterman, M Uddin - Proceedings of the …, 2021 - journals.sagepub.com
Simple reduced order models (ROMs) for the aerodynamic coefficients-lift, drag, and pitch
moment-of a pitching NACA0012 airfoil are presented. The ROMs are designed for quick …
moment-of a pitching NACA0012 airfoil are presented. The ROMs are designed for quick …
Aerodynamic cell design for air load measurements on high aspect ratio airfoils
H Fellouah - 2013 - sae.org
This study concerns the design of a three components internal aerodynamic cell. It will be
used to measure the lift, drag and pitching moment on static or oscillating airfoils enduring …
used to measure the lift, drag and pitching moment on static or oscillating airfoils enduring …
[引用][C] Analyse numérique de l'interaction fluide structure de l'écoulement de l'air autour d'une structure déformable
F ZIANE, A Abdellah El-hadj - 2018