Measurements of Unsteady Pressures and Wake Fluctuations for Flow Over a Cylinder at Supercritical Reynolds Number
<p>A test was conducted to measure and map the unsteady pressure fluctuations over the surface of a smooth, cantilevered, circular cylinder in the supercritical Reynolds number range from 2.5 x 10<sup>5</sup> to 7.5 x 10<sup>5</sup>. Lift fluctuations were measured, hot...
Internet
https://thesis.library.caltech.edu/265/1/Spitzer_re_1965.pdfSpitzer, Robert Edward (1965) Measurements of Unsteady Pressures and Wake Fluctuations for Flow Over a Cylinder at Supercritical Reynolds Number. Engineer's thesis, California Institute of Technology. doi:10.7907/WT4K-6337. https://resolver.caltech.edu/CaltechETD:etd-01222004-093919 <https://resolver.caltech.edu/CaltechETD:etd-01222004-093919>