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Aerodynamic forces acting on three circular cylinders having different diameters closely arranged in line
AbstractIn order to predict the aerodynamic forces by a strong wind acting on the H2 Rocket under development in Japan, experimental studies were carried out. A one-hundredth test model of the actual object is composed of a main circular cylinder and two subcylinders closely arranged in line. The pressure distributions around the cylinders and the Strouhal number behind the cylinders were measured for various attack angles α in the range of the subcritical Reynolds numbers. At α=22° and 33°, the drag and lift coefficients of the main cylinder and the individual subcylinders have either a maxima or minima. These phenomena are closely related to the reattachment of the separated shear layer from the upstream cylinder on the downstream cylinder.
Aerodynamic forces acting on three circular cylinders having different diameters closely arranged in line
AbstractIn order to predict the aerodynamic forces by a strong wind acting on the H2 Rocket under development in Japan, experimental studies were carried out. A one-hundredth test model of the actual object is composed of a main circular cylinder and two subcylinders closely arranged in line. The pressure distributions around the cylinders and the Strouhal number behind the cylinders were measured for various attack angles α in the range of the subcritical Reynolds numbers. At α=22° and 33°, the drag and lift coefficients of the main cylinder and the individual subcylinders have either a maxima or minima. These phenomena are closely related to the reattachment of the separated shear layer from the upstream cylinder on the downstream cylinder.
Aerodynamic forces acting on three circular cylinders having different diameters closely arranged in line
Igarashi, T. (Autor:in)
Journal of Wind Engineering and Industrial Aerodynamics ; 49 ; 369-378
01.01.1993
10 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 1993
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