1967
DOI: 10.1017/s002211206700031x
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Experiments on the low-speed flow past cones

Abstract: The wake behind a cone in incompressible flow has the form of a closed bubble. Measurements of velocity, turbulence and static pressure for various cone angles show that the wakes are all essentially similar. A wake Strouhal number may be defined, which is the same for all the models. A disk may be treated as a cone of 180° vertex angle.

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Cited by 101 publications
(48 citation statements)
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“…It was noted above that Calvert (1967a) studied wakes behind cones with axes parallel to the flow direction, apexes directed upstream, and various apex angles. Such wakes were investigated in more detail by Goldburg and Florsheim (1966) who observed wakes behind freely falling cones (with apexes directed downwards) together with wakes behind falling cone-spheres (hemispheres attached to the base of cones).…”
Section: Wakes Behind Spheres and Other Axisymmetric Bodiesmentioning
confidence: 99%
“…It was noted above that Calvert (1967a) studied wakes behind cones with axes parallel to the flow direction, apexes directed upstream, and various apex angles. Such wakes were investigated in more detail by Goldburg and Florsheim (1966) who observed wakes behind freely falling cones (with apexes directed downwards) together with wakes behind falling cone-spheres (hemispheres attached to the base of cones).…”
Section: Wakes Behind Spheres and Other Axisymmetric Bodiesmentioning
confidence: 99%
“…Many authors have studied these flows to investigate the effect of bluff-body geometry on flame stability (Beer and Chiger, 1983;Sivasegaram and Whitelaw, 1987;Durao and Whitelaw, 1978;Witerfeld, 1965;Bradbury, 1976;Calvert, 1967;Davis and Beer, 1971;Chiger and Beer, 1964). Several studies emphasized the effect of confinement on the nonreacting flow behind bluff bodies.…”
Section: Prior Confined Burner Studiesmentioning
confidence: 99%
“…Kim and Morris (2002) presented the numerical simulation of compressible inviscid mean flow pattern of a cone with 608 vertex angle. The results were compared to the experimental data, assessed by Calvert (1967). Sakai (2009) considered truncated cones to evaluate the CFD simulation of the drag performance of supersonic flow with repetitive energy depositions.…”
Section: Introductionmentioning
confidence: 99%