In the present paper, free surface vortex formation at intakes is investigated analytically. By assuming a spiral form for vortex streamlines, continuity and momentum equations were integrated and solved in a vortex flow domain. From this solution, velocity and pressure distributions were found above the intake under vortex action. An equation for the water surface profile was also found and compared with another research. By considering that in an air core vortex, pressure at the intake entrance drops to zero, a relationship was found for critical submerged depth and verified by experimental data and another analytical equation. It was concluded that the results of the proposed spiral analytical model had good agreement with the experimental data.

  • Analytical analysis of free surface vortex phenomenon over a vertical intake in the reservoir.

  • Solving 3D Navier-Stokes equations analytically for a swirling flow.

  • Predicting the critical submergence at a vertical intake.

  • Extracting pressures and velocities analytically using spiral theory.

  • Comparing obtained analytical results with previous experimental and analytical results.

The following symbols are used in this paper:

D

intake pipe diameter

Fr

intake Froude Number = V/√gD

Γ

vortex strength

NΓ

circulation number

g

gravitational acceleration

gr

gravitational acceleration in r direction

gz

gravitational acceleration in z direction

gθ

gravitational acceleration in θ direction

Re

intake Reynolds number = VD/

S

intake submerged depth

Sc

critical intake submerged depth

V

intake flow velocity

kinematic viscosity

ρ

density of water

σ

surface tension of water

r, θ and z

coordinate directions

r

distance from the vortex center

rm

radius at the maximum tangential velocity

Vθ

tangential velocity

Vr

radial velocity

Vz

velocity in the z direction

P

pressure

ω

Angular velocity

Vortices are often experienced in nature and industries; for example in the course of water withdrawing at intakes (Khanarmuei et al. 2016; Khadem Rabe et al. 2018; Tahershamsi et al. 2018; Pakdel et al. 2020) and may be important for the desalination and treatment of saline wastewater (Panagopoulos et al. 2019; Panagopoulos & Haralambous 2020; Panagopoulos 2021). In spite of their common occurrence, vortex structure, formation and dynamics, are still not completely understood (Stepanyants & Yeoh 2008). Many factors affect on vortex formation and flow field near the intake structure such as asymmetry in the inflow and reservoir geometry (Roshan et al. 2009; Amiri et al. 2011; Sarkardeh et al. 2012; Sarkardeh et al. 2013), flow velocity in the intake, submerged depth and diameter of the intake pipe. Study of free surface vortices is important and necessary not only from a purely academic view, but also for a better understanding of such fluid phenomena in practical engineering systems. Most vortices in nature, however, have a ‘spatial’ structure; that is, the streamlines are not perpendicular to the axis of rotation (Lugt 1983). There are visual evidences as well as computational simulations that show the vortex streamlines follow a spiral path (Lugt 1983; Shukla & Kshirsagar 2008; Lucino et al. 2010; Sarkardeh et al. 2014). A schematic and real spiral vortex are presented in Figure 1(a) and 1(b) respectively.

Figure 1

Spiral streamlines in a vortex (a) from Lugt (1983) and (b) from WRI (1992).

Figure 1

Spiral streamlines in a vortex (a) from Lugt (1983) and (b) from WRI (1992).

Close modal

One important case in engineering practice is withdrawing water at intakes. Surface vortex formation at intakes is an undesirable phenomenon, causing air entrainment into the intake, vibration and energy loss (Knauss 1987). Vortices can be divided into six types based on visual classification at the Alden Research Laboratory (Padmanabhan & Hecker 1984). Type 1 is observed as a weak rotation of flow at the water surface. In Type 2, in addition to water surface rotation, a dimple is also observed at the water surface. In Type 3, the rotation of the flow extends down to the intake itself. In Type 4, debris is dragged into the intake. In Type 5, some air bubbles are entrained from the water surface and are transported down to the intake. In the strongest surface vortex (Type 6), a stable air core is formed in the center of the vortex and air is steadily entrained into the tunnel (Knauss 1987). To prevent air entrainment of surface vortices, a minimum submerged depth of the intake, called the critical submerged depth Sc, is recommended for the intake (Figure 2(a)). Submerged depth is defined as the vertical distance between the water surface and the level of the intake center (Figure 2(b)).

Figure 2

Schematic view of an intake and parameter definitions (a) with an air core vortex (b) without vortex.

Figure 2

Schematic view of an intake and parameter definitions (a) with an air core vortex (b) without vortex.

Close modal

Vortex phenomenon is studied with three different possible approaches: i-experimentally, ii-numerically and iii-analytically. In the experimental studies, a physical model has been constructed so that the scale effects were minimized. Vortices were then studied in different hydraulic and geometric conditions and related hydraulic factors were measured. By collecting data, empirical equations have been developed and proposed for practical hydraulic designs such as for critical submerged depth (Denny & Young 1957; Berge 1966; Gordon 1970; Reddy & Pickford 1972; Amphlett 1976; Chang 1977; Anwar et al. 1978; Jain et al. 1978; Sarkardeh et al. 2010; Amiri et al. 2011). In numerical studies, by discretizing governing equations, flow motion equations have been solved for the flow domain. Results also have been verified by experimental data. The results of this approach could help future simulations and prevent extra costs in physical modeling (Constantinescu & Patel 1998, 2000; Marghzar et al. 2003; Shukla & Kshirsagar 2008; Lucino et al. 2010; Sarkardeh et al. 2014). There have been also several attempts at analytical solution of vortex at intakes (Rott 1958; Lundgren 1985; Miles 1998; Andersen et al. 2003, 2006; Lautrup 2005; Stepanyants & Yeoh 2008; Yildirim et al. 2012; Schneider et al. 2015).

Maybe the first analytical study on vortex was done by Rankine (1858). He suggested a simple model for analyzing an intake vortex. In his proposed model the inner core is assumed as a forced and the outer region as a free vortex. The boundary between the forced inner and irrotational outer free vortex is located at a distance equal to the radius of the intake from the axis of rotation. In the Rankine (1858) Model the velocity component in z direction is ignored and streamlines are considered as concentric circles. Rankine (1858) also defined vortex strength by its circulation as (White 2003):
formula
(1)
formula
(2)
where Γ is vortex strength, ω is angular velocity and Vθ is the tangential velocity at a distance r from the vortex axis. It is obvious that Γ is constant in the irrotational part of the vortex and ω is constant in the forced part of the vortex.
Another analytical attempt to describe the vortex phenomenon and calculate the critical submerged depth was made by Odgaard (1986). He suggested a model which provided a reasonable relationship between the critical submerged depth (Sc see in Figure 2(a)) and flow parameters such as discharge, circulation, viscosity and surface tension. Odgaard (1986) model was based on exact solution of governing equations for viscous unbounded fluid. Odgaard (1986) assumed the flow situation as steady, axi-symmetric, incompressible and the radial velocity component nearly linear near the pipe entrance. He also, by integrating equations of motion and Navier-Stokes, developed the following equation without the surface tension term for calculating critical submerged depth:
formula
(3)

Many simplifying assumptions were made to derive Odgaard (1986) equations.

In the present paper, by applying spiral form for vortex streamlines in continuity and momentum equations, governing equations in complete form were integrated and 3D flow domain was solved in the presence of an air core vortex. The critical submerged depth was then determined by implementing independent non-dimensional parameters. Moreover, the water surface and formed air core were plotted regarding the extracted equations from the spiral analytical model. Finally, proposed equations were compared with other researcher results.

The governing continuity and Navier–Stokes equations describing flow in a steady state incompressible fluid are given by the following set of equations (White 2003):
formula
(4)
formula
(5)
formula
(6)
formula
(7)
where Vr, Vz and Vθ are the radial, axial and tangential components of the velocity field; g is the acceleration due to the gravity; ρ is the fluid density; p is the pressure; and is the kinematic viscosity. A spiral path in space in cylindrical coordinate scan be described by the following equations:
formula
(8)
formula
(9)
formula
(10)
where a, b and c are the controller coefficients to produce different spiral curves. Few spirals are plotted in Figure 3 using Equations (8)–(10).
By differentiating Equations (8)–(10) and using Vr = dr/dt, Vz = dz/dt, Vθ = rdθ/dt flow velocity components can be written as:
formula
(11)
formula
(12)
formula
(13)
Figure 3

Typical spiral curves using Equations (8)–(10).

Figure 3

Typical spiral curves using Equations (8)–(10).

Close modal
Along the streamlines one can write (Li & Lam 1964):
formula
(14)
formula
(15)
formula
(16)

Substituting Equations (11)–(13) into Equations (14)–(16) confirms their correct expressions for velocity components. In addition the relationship found between velocity components in a spiral path (Equations (11)–(13)), satisfy the continuity Equation (4) too.

Free vortex region

Applying Equation (1) in Equations (11)–(13), and using Equations (8)–(10), tangential, axial and radial velocity components can be written as:
formula
(17)
formula
(18)
formula
(19)

One can plot spiral streamlines and velocity vectors from Equations (17) to (19) (Figure 4). For example by assuming Γ = 0.4 and θ between zero and 2π, three streamlines are plotted in Figure 4(a). 2D plot of these streamlines in xy plane is shown in Figure 4(b) and vector plot of xy component of velocity vector is also plotted in Figure 4(c).

Figure 4

Typical spiral streamlines and velocity vectors using Equations (17)–(19). (a) 2D streamlines. (b) 2D Velocity Vectors. (c) 3D Streamlines.

Figure 4

Typical spiral streamlines and velocity vectors using Equations (17)–(19). (a) 2D streamlines. (b) 2D Velocity Vectors. (c) 3D Streamlines.

Close modal

Integrating navier-stokes equations for pressure distribution at free vortex region:

The origin of the cylindrical coordinate system (r, z, θ) was considered at the reservoir surface, and the z-axis directed downwards (Figure 2). Substituting Equations (17)–(19) in Equations (5)–(7) and integrating them yields:

In r direction:
formula
(20)
formula
(21)
Indirection:
formula
(22)
formula
(23)
In z direction:
formula
(24)
formula
(25)
where C1, C2 and C3 are constants.
By considering:
formula
(26)
Therefore:
formula
(27)
where Pr, Pθ and Pz are the integrated pressure equations along the r, θ and z respectively. Finally, pressure distribution is:
formula
(28)
where C equals to zero in case of no vortex (Γ = 0 → P = ρgz).

Forced vortex region

At forced vortex region by applying Equation (2) in Equations (11)–(13), and using Equations (8)–(10), tangential, axial and radial velocity components can be written as:
formula
(29)
formula
(30)
formula
(31)

Spiral streamlines and velocity vectors were plotted from Equations (29) to (31) in Figure 5 as well as assumptions for plotting Figure 4.

Figure 5

Typical spiral streamlines and velocity vectors using Equations (29)–(31). (a) 2D streamlines. (b) 2D velocity vectors. (c) 3D streamlines.

Figure 5

Typical spiral streamlines and velocity vectors using Equations (29)–(31). (a) 2D streamlines. (b) 2D velocity vectors. (c) 3D streamlines.

Close modal

Integrating Navier-Stokes equations for pressure distribution at forced vortex region:

The origin of the cylindrical coordinate system (r, z, θ) was considered at the reservoir surface, and the z-axis directed downwards (Figure 2). Substituting Equations (29)–(31) in Equations (5)–(7) and integrating them yields:

In r direction:
formula
(32)
formula
(33)
In direction:
formula
(34)
formula
(35)
In z direction:
formula
(36)
formula
(37)
where C1, C2 and C3 are constants.
By considering:
formula
(38)
Therefore:
formula
(39)
where Pr, Pθ and Pz are the integrated pressure equations along the r, θ and z respectively. Finally, pressure distribution is:
formula
(40)
where C equals to zero in case of no vortex (ω = 0 → P = ρgz).
The surface profile of a vortex derived through considering P equal to zero at Equations (28) and (40) for free and forced vortex regions respectively and neglecting viscosity due to its small effect (Hite & Mih 1994):
formula
(41)
where H is the water surface, C is the constant coefficient, a1 is 3Γ2/θ2r4 and a2 is (9θ2Γ2 + 3Γ2)/θ2r2. For example in Figure 6, Equations (41)a and (41)b is plotted for Γ = 0.4, ω = 2.5, g = 9.81, π = 3.14 and C = -0.081.
Figure 6

Water surface profile (cm). (a) 3D view. (b) 2D side view. (c) 2D plane view.

Figure 6

Water surface profile (cm). (a) 3D view. (b) 2D side view. (c) 2D plane view.

Close modal
To find the radius at the maximum tangential velocity (rm) which demarcates the inner core and outer zone of vortex, Equations (1) and (2) was used.
formula
(42)
Hite & Mih (1994) proposed an equation for predicting free surface profile of a vortex:
formula
(43)
where H0 is the water surface elevation at the center. The result of spiral model for free surface profile was compared with Hite & Mih (1994) equation (Equation (43)) in Figure 7.
Figure 7

Comparison of free surface profile between Spiral Model and Hite & Mih (1994).

Figure 7

Comparison of free surface profile between Spiral Model and Hite & Mih (1994).

Close modal

As can be seen from Figure 7, spiral model predicts water surface profile trend as same as Hite & Mih (1994) with maximum difference in water depth about 20%.

To calculate critical submerged depth, a vertical intake is considered (Figure 2). When a Type 6 vortex forms at an intake and the air core reaches the intake entrance (Figure 2(a)), pressure at the intake entrance will be atmospheric (equal to zero). If such a boundary condition is used in Equation (28) the Equation (44) is derived:
formula
(44)
where Fr is Froude Number (=V/g1/2D1/2), Re is Reynolds Number (=VD/), S/D is relative submerged depth and NΓ is Circulation Number (=Γ/2πg1/2D3/2). If viscosity is neglected in the region of free surface vortex, Equation (44) is simplified and solved for Sc/D as:
formula
(45)

Equation (45) has one real and two unreal roots and can be analytically solved for S/D. It should be noted that to calculate the critical submergence in the present analytical model, the boundary between force and free vortex region at the intake entrance was considered equal to D/4. To verify Equation (45), experimental results of Paul (Odgaard 1986) and analytical equation of Odgaard (1986) was utilized. Paul (Odgaard 1986) measured critical submerged depth at a vertical intake (Table 1).

Table 1

Experimental data of Paul (Odgaard 1986) on an air core vortex in a vertical intake

Intake velocity V (m/s)Intake pipe diameter D (m)Vortex strength Γ (m2/s)Critical submerged depth Sc (m)
0.241 0.1528 0.3600 0.72 
0.417 0.1528 0.4700 1.25 
0.370 0.0663 0.1384 0.50 
1.336 0.0160 0.0184 0.42 
0.259 0.1017 0.2289 0.52 
0.510 0.0383 0.0680 0.43 
0.707 0.0288 0.0420 0.41 
Intake velocity V (m/s)Intake pipe diameter D (m)Vortex strength Γ (m2/s)Critical submerged depth Sc (m)
0.241 0.1528 0.3600 0.72 
0.417 0.1528 0.4700 1.25 
0.370 0.0663 0.1384 0.50 
1.336 0.0160 0.0184 0.42 
0.259 0.1017 0.2289 0.52 
0.510 0.0383 0.0680 0.43 
0.707 0.0288 0.0420 0.41 

The prediction of the present spiral model (Equation (45)) for critical submerged depth is compared with experimental data of Paul (Odgaard 1986) in Figure 8. Results of Odgaard (1986) equation (Equation (3)) are also shown in this figure.

Figure 8

Comparison between results of the present spiral model for critical submerged depth with experimental data of Paul (Odgaard 1986) and analytical model of Odgaard (1986).

Figure 8

Comparison between results of the present spiral model for critical submerged depth with experimental data of Paul (Odgaard 1986) and analytical model of Odgaard (1986).

Close modal

As can be seen from Figure 8, Odgaard (1986) over estimated S/D with a different trend compared to the experimental data. Figure 8 shows that the results of the present analytical study are near to the experimental data and with a similar trend.

In the present analytical study, a spiral model for vortex flow was introduced. In this model, the spiral equations were applied in the 3D cylindrical Navier-Stokes equations. After substituting, differentiating and integrating equations, velocity and pressure distributions and also fluid surface profile were yielded. For a practical verification, an air core vortex as a critical state at intakes was selected. Water surface of an air core free surface vortex was plotted and compared with Hite & Mih (1994) proposed equation and the deviation was found to be about 20% in the maximum point. Using the present spiral model, an equation for critical submerged depth was derived and compared with experimental data of Paul (Odgaard 1986) and analytical equation of Odgaard (1986). Results showed that present spiral model could predict (S/D)cr in good agreement with experimental data.

All relevant data are included in the paper or its Supplementary Information.

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