Phenomenological study of the interactions between...

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Multiphase 2017 ENS Cachan, France 16 th October 2017 (a) (b) (c) (d) Phenomenological study of the interactions between pressure waves and development of jets for simplified liquid impacts N. Couty (a) , Y. Jus (a) , P.-M. Guilcher (b) , L. Brosset (c) , D. Le Touzé (d)

Transcript of Phenomenological study of the interactions between...

Page 1: Phenomenological study of the interactions between ...intranet.ens-paris-saclay.fr/colloque-cmla... · ELP2 may be compressible before getting incompressible (1) Rochester M. C. (1977).

Multiphase 2017 – ENS Cachan, France – 16th October 2017

(a) (b) (c) (d)

Phenomenological study of the interactions between pressure waves and development of

jets for simplified liquid impacts

N. Couty (a), Y. Jus (a), P.-M. Guilcher (b), L. Brosset (c), D. Le Touzé (d)

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Outline

► Introduction

► Flat impact of liquid on rigid wall without gas

► Impact of curved liquid domain on rigid wall without gas

►Conclusion

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Introduction

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Context

Impact of LNG on insulated walls of tanks due to sloshing

Impact of a plunging wave on corrugations (Sloshel project)

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Visualization of compressible effects in the

liquid

Experimental (Sloshel project)

« Flip through » impact

High pressure peaks weremeasured in some cases

Numerical (SPH-flow)

« Large gas pocket » impact

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Sequence of phenomena

Building jetBuilding jet

Direct impact Jets

time

Incom

pre

ssib

le

ga

sflow

Escape of the gas

Closure of the gas pocket

Impact of the crest

Compression of the gas pocket

Flaring of the impacted crest

Compressed gas pocket

Sloshel project

SPH-flowbi-fluid

Vertical velocity field Pressure field Pressure field

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Elementary Loading Processes (ELPs)

« Pressure surface »:

time-spacedistribution of

pressure on the wall

y

t

Impact

Pre

ss

ure

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Canonical models of the ELPs

Direct impact (ELP1)

Liquidcompressibility

Compressed gas (ELP3)

Gascompressibility

Building jet (ELP2)

Liquidmomentum

Canonical models

Scalinglaws

ELP

Mach (liquid) Froude Mach (gas)

0p U

Rankine and Hugoniot Wagner

p0p U

Bagnold

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Subject of the study

Transition between ELP1 and ELP2

► This phase seems to provide high pressures potentially important for design

► Very small scales of time and space involved numerical models must be adapted

Pressure field inside the fluids

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Purpose of the study

Questions to be answered

►Pressure levels and duration of initial peaks (with accuracy)?

►Canonical solution: simply sum ELP1 + ELP2 or coupled brick ?

►Consequence on scaling rules?

Scope of work

►Means:

Numerical simulation:

• SPH method (SPH-flow)• Eulerian Finite Elements (LS-Dyna)

Look at theoretical works

►Studied case:

Idealization of the crest by a patch with constant

curvature front

V0

No gas

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Infinite R

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Characteristics of the test

V0

►Aspect ratio: L/H = 1/8

►Mass density: r = 455 kg/m3

►Celerity of sound: c = 1300 m/s

► Impact velocity: V0 = 6.26 m/s (corresponds to a drop of 2 m)

►Acoustic pressure: rcV0 = 37 bar

H

L

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Reminder of the results in 1D

V0

V0

P = 0

V = 0

P = rcV0

c

t = 0

P = 0

t > 0

Propagation of a compression shock wave at the celerity of sound

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Pressure field in the liquid

Acoustic pressure:ρcV0 = 37 bar

SPH-flow computationHalf model

The compression shock wave with flat frontcombines with

a relaxation shock wave with circular frontarising from the corners

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Pressure field in the liquid (later time)

► Flat compression wave P1

𝑝1 𝑥, 𝑦, 𝑡 =

0 𝑓𝑜𝑟 𝑡 < 𝑦/𝑐

𝑝𝑎 𝑓𝑜𝑟𝑦

𝑐≤ 𝑡 ≤

2𝐻 − 𝑦

𝑐

0 𝑓𝑜𝑟 𝑡 >2𝐻 − 𝑦

𝑐

► Circular relaxation wave P2

𝑝2 𝑥, 𝑦, 𝑡 =0 𝑓𝑜𝑟 𝑡 <

(𝐿 − 𝑥)2+𝑦2

𝑐

−𝛼 𝑡 . 𝑝𝑎 𝑓𝑜𝑟 𝑡 ≥(𝐿 − 𝑥)2+𝑦2

𝑐

► Circular relaxation wave P3

𝑝3 𝑥, 𝑦, 𝑡 =0 𝑓𝑜𝑟 𝑡 <

(𝐿 + 𝑥)2+𝑦2

𝑐

−𝛼 𝑡 . 𝑝𝑎 𝑓𝑜𝑟 𝑡 ≥(𝐿 + 𝑥)2+𝑦2

𝑐

x

y

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Time-space pressure distribution on the wall:

p(x/L, 0, t)

► Perspective ► Top view

P(x/L, 0, 0)

P = P1(x, 0, t) = Pa

t1 = (L-x)/c

t2 = (L+x)/c

P = P1+P2= Pa (1-a(t))

P = P1+P2+P3

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Finite R

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R R-v0t

h = v0t C

v0

vc

rc

V0

Displacement of the geometrical contact

point

► Displacement of the geometrical

contact point assuming 𝑉0𝑡 ≪ 𝑅 (smallvertical displacement w.r.t. R):

𝑟𝑐 𝑡 ≈ 2𝑅𝑉0𝑡

► Speed of the geometrical contact point:

𝑉𝑐 𝑡 ≈𝑅𝑉0

2𝑡⇒ Firstly, 𝑉𝐶 ≫ 𝑐

R

Propagation of contact pointsVc

► Existence of a critical time 𝑡𝑐𝑟 ≈𝑅𝑣0

2𝑐2after which 𝑉𝑐 < 𝑐

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Pressure field in the liquid column

timeSPH-flow computation

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Acoustic phase (compressible, ELP1)

► As long as 𝑽𝒄 > 𝒄:

Purely acoustic phase

The jet cannot start

Succession of impacts at the contact point:

time

Pressure

Vertical velocity

2 instants

(1) Knežević K. H. (1972). High-velocity impact of a liquid droplet on a rigid surface: the effect of liquid compressibility. Dissertation submitted to the Swiss Federal Institute of Technology Zurich for the degree of Doctor of Technical Sciences.

Shock front as envelope of superposedcircular waves (1)

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Jet phase (incompressible?, Wagner, ELP2)

►From 𝒕 > 𝒕𝒄𝒓 (𝑽𝒄 < 𝑪):

Relaxation wave from critical point

The jet can build up

time

Rein M. (1993). Phenomena of liquid drop impact on solid andliquid surfaces. Fluid Dynamics Research, vol. 12, pp 61-93.

Pressure

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Birth of the jet (numerical…)

time

Horizontal velocity field (SPH-flow)

Pressure (SPH-flow)

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What we had in mind!

(1) Faltinsen O. M. (1990). Sea loads on ships and offshore structures. Cambridge University Press.

Pressure field measured in experimental impact of a cylinder (1)

Max. pressure = acoustic pressure

Experiment

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Time-space pressure distribution on the wall

Zoom:

►The acoustic pressure is here

►And it is exceeded!

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Top view

Geometrical / numerical positions of the contact point

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Existing works

►Some references in the litteratureabout the impact of droplets

►But lack of formulation describing the whole ELP1+ELP2 phenomenon

►ELP2 may be compressible beforegetting incompressible

(1) Rochester M. C. (1977). The impact of a solid drop with a solid surface. University of Cambridge.

Pressure field at the wall at different time instants (1)

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Conclusion

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How the pressure field on the wall might look

like

(1) Faltinsen O. M. (1990). Sea loads on ships and offshore structures. Cambridge University Press.

Pressure field measured in experiment of impact of a rigid cylinder (1)

?

►Observed with two codes in the study

►Some theoretical works in the litterature

Acoustic pressure

Experiment:

► Was it able to measurehigh pressure peaks?

► Influence of the air?

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Conclusion

►Pressure on the wall exceeds rcV0 ! :

Rather unexpected

Be careful: potentially very short in time and concentrated in space

►References found in the litterature (impact of droplets, Koropkin, etc.)

►Phenomenology to complete

►Now we have to go deeper in the formulations:

ELP1: analytical model possible

ELP2: « compressible Wagner theory »?

►Aim unchanged:

Canonical model to represent this phase by locally approaching the crest free surface by a constant curvature

Scale rules

►Perspectives :

Addition of model of local small gas pocket in the crest

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Thank you for your attention

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