cfd study of the flow in the vicinity of a subsea pipeline khalid m. saqr, mohamed saber, amr a....

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CFD Study of the Flow in the Vicinity of a Subsea Pipeline Khalid M. Saqr, Mohamed Saber, Amr A. Hassan, Mohamed A. Kotb College of Engineering and Technology Arab Academy for Science, Technology and Maritime Transport 1029 Abu Qir, Alexandria – EGYPT [email protected]

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CFD Study of the Flow in the Vicinity of a Subsea Pipeline

Khalid M. Saqr, Mohamed Saber, Amr A. Hassan, Mohamed A. Kotb

College of Engineering and TechnologyArab Academy for Science, Technology and Maritime

Transport1029 Abu Qir, Alexandria – EGYPT

[email protected]

1. Problem outlines

• Subsea pipelines are subjected to hydrodynamic stresses due to marine currents

• These stresses may rupture the pipeline and cause financial losses and environmental hazards.

• There is a demand to improve the methods used to protect subsea pipelines from hydrodynamic stresses

• This paper presents a comparison between two protection methods.

1. Problem Outlines

• Current protection methods– Trenching/Burying the pipeline into seabed.– Concrete weight coating.– Concrete mattress adding.– Rock dumping (covering).

1. Problem Outlines

• The proposed double barrier method

Pipeline

Barrier

Seabed

2. Methodology: Physical Model

• Computational Fluid Dynamics (CFD) model

Trenching method

Double barrier method

a

b

α ranges from 0.1 to 0.75

XY

L

HU

Trench in seabed

b

a

Pipeline

Barrier

Seabedb

a

2. Methodology: CFD Approach

A survey of relevant literature showed that the current approaches involve:

1. Two and three dimensional models

2. Finite volume framework

3. RANS turbulence models

2. Methodology: Governing Equations

• Continuity: (1)

• Momentum: (2)

• Reynolds stress closure: (3)

• Turbulence models:– k – ε model

Turbulence kinetic energy

(4)

0

i

i

x

U

ijji

ijijj

Sxx

PuuUU

x 2

ijijTij kSuu

3

212

2Sk

xxkU

x Tjk

T

ji

i

2. Methodology: Governing Equations

turbulence dissipation rate

(5)

– Eddy viscosity Cμ = 0.09

– Realizable k-ε model

(6)

k

CSk

Cxx

Ux T

j

T

ji

i

2

22

1

kCSC

xxU

x j

T

ji

i

2

21

5

,43.0max1

C

kUAA s

0

1C ijijijijSSU *

2kCT

WAs 6arccos

3

1cos6 3

8

S

SSSW kijkij

i

j

j

iij x

u

x

u

2

1

2. Methodology: Governing Equations

– k-ω turbulence model

– SST k-ω turbulence model

A hybrid model which applies the standard k-ε model in the near wall region and k-ω in the main stream region

kUx

kxx

kx

U ii

ijj

Tji

i**

2

ij

ijj

Tji

i Uxkxxx

U

kT

9

5

40

3

100

9* 2

1*

2. Methodology: CFD Model Reliability Check

Elementary computational model

Different grid resolutions

Compare flow field obtained by different grids

Predictions agree ?

Refine grid resolution

NO

Select the optimum grid

YES

VERIFICATION

Test turbulence model

Best agreementwith measurements ?

NO

Change model

Select best turbulence model

Optimize numerical scheme

VALIDATION

Final Computational Model

2. Methodology: Validation

•CFD Model Validation

Comparison between CFD predicted pressure coefficient using four turbulence models and experimental measurements of [9] on the pipe wall.

2

2

1U

PPC p

3. Results: Flow structureα = 0

0.0 0.3 0.6 0.9 1.2 1.5

α = 0 0o

90o

180o

270o

Flowdirection

Figure 5. Contours of normalized velocity magnitude and vectors over a bare pipe

Flow structure of the bare pipe

3. Results: Flow structureα = 0.1

α = 0.25

α = 0.5

0.0 0.3 0.6 0.9 1.2 1.5

α = 0.25

α = 0.1

α = 0.75

α = 0.5

α = 0.75

3. Results: α = 0.1

3. Results: α = 0.25

3. Results: α = 0.5

3. Results: α = 0.5

4. Conclusions

1. It can be concluded that the double barrier method is a prospective alternative to trenching at small aspect ratios.

2. With the difficulties faced during the trenching process, especially when the pipeline route passes a rocky terrain, the double barrier method appears as an efficient and reliable alternative.

3. The present work also reveals that the low-Reynolds number turbulence models (k-ω) performs better than the high-Reynolds number models in the present problem.

4. With proper construction of the non-uniform grid, a number of cells as small as 3×104 can be sufficient to produce accurate results.