Drag of Circular Cylinders for a Wide Range of Reynolds Numbers and Mach Numbers

195362 citationsJournal Articlegreen Open Access

Authors

Abstract

From Summary: "Pressure distributions around circular cylinders placed perpendicular to the stream for subsonic and supersonic flow conditions have been obtained. Drag coefficients calculated from these wind-tunnel tests and from transonic free-flight tests are presented. Drag data are presented for the Mach number range of 0.3 to 2.9."

Topics & Keywords

Fluid Dynamics and Turbulent Flows Fluid Dynamics and Vibration Analysis Aerodynamics and Fluid Dynamics Research

UN Sustainable Development Goals

Affordable and clean energy

Publication Details

Published in: University of North Texas Digital Library (University of North Texas)

Field-Weighted Citation Impact: 0.00