1999
DOI: 10.1063/1.869909
|View full text |Cite
|
Sign up to set email alerts
|

Spanwise structure of wall pressure on a cylinder in axial flow

Abstract: The spanwise structure of wall pressure fluctuations was measured in an axisymmetric turbulent boundary layer on a cylinder parallel to the mean flow at a momentum thickness Reynolds number of 2530 and a boundary layer thickness to cylinder radius ratio of 4.81. The measurements were made using miniature hearing aid type condenser microphones with spanwise separations of 0°, 10°, 20°, 30°, 60°, and 90°. An improved wall pressure power spectrum was obtained at low frequencies by utilizing a two-point subtractio… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
2
1

Citation Types

1
9
2

Year Published

2002
2002
2024
2024

Publication Types

Select...
7

Relationship

0
7

Authors

Journals

citations
Cited by 14 publications
(12 citation statements)
references
References 32 publications
1
9
2
Order By: Relevance
“…point wall pressure (table 5) closely match those of . Snarski & Lueptow (1995) and Bokde et al (1999) performed experiments at similar Reynolds numbers to those considered here. Snarski & Lueptow (1995) give a point r.m.s.…”
Section: 3mentioning
confidence: 99%
See 3 more Smart Citations
“…point wall pressure (table 5) closely match those of . Snarski & Lueptow (1995) and Bokde et al (1999) performed experiments at similar Reynolds numbers to those considered here. Snarski & Lueptow (1995) give a point r.m.s.…”
Section: 3mentioning
confidence: 99%
“…Snarski & Lueptow (1995) give a point r.m.s. wall pressure measurement (scaled on ρU 2 0 ) of 4.32 × 10 −3 for Re = 3644 for δ = 5, and Bokde et al (1999), 4.63 × 10 −3 for Re = 3300 for δ = 4.81. These are consistent with the values obtained here (table 5).…”
Section: 3mentioning
confidence: 99%
See 2 more Smart Citations
“…According to Bokde et al (1999), the turbulent boundary layer on a cylinder in axial flow is not significantly different from that on a flat plate when the boundary layer thickness is of the same order or smaller than the radius of the cylinder. For a cylindrical geometry the turbulent structures are not bounded in the span-wise direction, and are free to move around the streamer.…”
Section: The Acoustic Source Termmentioning
confidence: 99%