On quasi-steadiness of transverse galloping of rectangular cylinders at Reynolds numbers below 10,000

Author:

Naguib Ahmed M.,Feero Mark A.,Safaripour AlirezaORCID,Koochesfahani Manoochehr M.

Funder

Army Research Office

Publisher

Elsevier BV

Reference36 articles.

1. A study of the aerodynamics of a low Reynolds number airfoil translating across a uniform-shear approach flow;Albrecht,2019

2. Single-component molecular tagging velocimetry of the boundary layer on a NACA-0012 airfoil plunging across uniform-shear flow;Albrecht,2020

3. Reynolds number and freestream shear effects on a NACA 0012 airfoil in the Reynolds number Range 10,000-30,000;Albrecht,2022

4. An Experimental Study of the Steadily Plunging Airfoil in Uniform-Shear Flow;Albrecht,2022

5. Experiments on flow-induced vibration of a square cylinder;Bearman;J. Fluids Struct.,1987

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