Single-stream swirling jet in still air.
Swirl number: \(S = G_{\theta}/(RG_{x}) = 0.36\) where \(G_x\) and \(G_{\theta}\) are the axial and angular momentum fluxes, and \(R\) the incoming pipe radius.
Exit Reynolds number: \(Re = 56,000\)
The addition of swirl has large-scale effects on free jet development. In particular, the rate of mixing in-creases with swirl intensity. Thus swirling jets spread more quickly, and the mean velocities decay more rapidly than in a non-swirling jet. In a strongly swirling jet the gradients of static pressure set up across the flow field introduce adverse axial pressure gradients in the region of swirl decay, and these may be strong enough to cause reversal of the forward velocities near the jet axis. Thus a re-circulation zone is set up downstream of the jet orifice. Weaker swirl leads to less strong curvature of the stream lines, and the flow is then amenable to analysis as a thin shear layer. Even so, the spreading rate may reach as much as twice that of a non-swirling jet. The enhanced mixing resulting from the adverse pressure gradient leads to increases in the turbulence intensities. Further downstream, where the swirl field is weakened, the turbulence levels and the spreading rate reduce approximately to those of the non-swirling jet.
In this experiment values of \(U\), \(V\), \(W\) and all \(\overline{u_iu_j}\) were measured for swirl numbers: \(S = 0\) and \(S = 0.36\) for downstream distances up to \(x/D = 6\). The external field was stationary. This test case involves the theoretical and experimental comparison between the variation of the centre-line values of \(U\), \(\overline{u^2}\) and \(\overline{v^2}\) with \(x/D\), as well as the decay of the maximum swirl velocity.
For comparison, a number of experimental investigations of free-swirling flows, including the present one, are summarized in the table below.
Author(s) | Method of Swirl Generation | Measurement Technique | Range of Axial Distance | Range of Swirl Number | Recirculation? | Measured Quantities |
---|---|---|---|---|---|---|
Rose (1962) | rotating pipe | hot-wire | 0.235-15.0 | 0-0.23 | No | \(U\), \(V\), \(W\), all normal stresses |
Chigier and Beer (1964) | tangential ports | impact probe | 0-0.6 | 0.39-1.43 | Yes | \(U\), \(W\) |
Keer and Fraser (1965) | vanes | impact probe | 11.7-19.0 | 0-0.72 | No | \(U\), \(V\), \(W\) |
Chigier and Chervinsky (1967) | tangential ports | impact probe | 1.0-15.0 | 0.13-0.66 | Yes | \(U\), \(W\), \(P\) |
Mathur and MacCallum (1967) | vanes | impact probe | 0.6-20.0 | 0-2.7 | Yes | \(U\), \(W\), \(P\) |
Maier (1967) | vanes | impact probe | 0.27-30.0 | 1.75-2.9 | Yes | \(U\), \(W\) |
Craya and Darrigol (1967) | tangential ports | hot-wire | 1.0-15.0 | 0-1.58 | Yes | \(U\), \(V\), \(W\), all \(\overline{u_iu_j}\) |
Syred, Beer and Chigier (1971) | tangential ports | hot-wire | 0-2.0 | 2.2 | Yes | \(U\), \(W\), \(\overline{u^2}\), \(\overline{v^2}\), \(\overline{w^2}\), \(\overline{uw}\) |
Kawaguchi and Sato (1971) | tangential ports | hot-wire | 0.1-4.0 | 0.6-0.9 | Yes | \(U\), \(W\), \(P\), all normal stresses |
Pratte and Keffer (1972) | rotating pipe | hot-wire | 1.0-30.0 | 0.3 | No | \(U\), \(W\), all \(\overline{u_iu_j}\) |
Hösel (1978) | tangential ports | LDA | 0.25-40.0 | 0-1.7 | Yes | \(U\), \(V\), \(W\) all \(\overline{u_iu_j}\) |
Fornoff (1978) | tangential ports | LDA | 0.25-40.0 | 0.53 | No | \(U\), \(V\), \(W\) all \(\overline{u_iu_j}\) |
Hellat (1979) | tangential ports | hot-wire; impact probe | 0.56-2.79 | 0-2.28 | Yes | \(U\), \(V\), \(W\) all \(\overline{u_iu_j}\) |
Ribeiro and Whitelaw (1980) | tangential ports | hot-wire | 0-6.0 | 0.32 | No | \(U\), \(V\), \(W\) all \(\overline{u_iu_j}\) |
Morse (1980a) | tangential ports | hot-wire | 0.5-20.0 | 0-0.40 | No | \(U\), \(V\), \(W\) all \(\overline{u_iu_j}\) |
Measurements available for the swirling case include:
Sample plots of selected quantities are available.
The data can be downloaded as compressed archives from the links below, or as individual files.
morse0.dat contains the development of centreline velocity, maximum swirl velocity and jet halfwidth along the jet. The files containing cross-jet profiles are given in the table below.
Streamwise location | File |
---|---|
\(x/D=0.5\) | morse1.dat |
\(x/D=1.0\) | morse2.dat |
\(x/D=2.0\) | morse3.dat |
\(x/D=4.0\) | morse4.dat |
\(x/D=6.0\) | morse5.dat |
\(x/D=10.0\) | morse6.dat |
Indexed data:
case026 (dbcase, free_flow) | |
---|---|
case | 026 |
title | Single-Stream Swirling Jet in Still Air |
author | Morse |
year | 1980 |
type | EXP |
flow_tag | axisymmetric, jet, swirl |