Download presentation

Presentation is loading. Please wait.

1
**Nathan N. Lafferty, Martin L. deBertodano,**

RELAP5 Analysis of Two-Phase Decompression and Pressure Wave Propagation Nathan N. Lafferty, Martin L. deBertodano, Victor H. Ransom Purdue University November 18, 2008

2
**Single-phase simulation benchmarked analytically **

Demonstrate capability of RELAP5 to model single and two-phase wave propagation (fast transients) Use of fine temporal and spatial discretizations Single-phase simulation benchmarked analytically Two-phase simulation compared to experiment Takeda and Toda experiment RELAP5 uncertainties for fast transients Steady-state interfacial area and heat transfer Choked flow model at low pressure Steady-state and fully developed flow interphase drag correlation ……

3
**Depressurization in Nuclear Systems**

Depressurization and propagation of rarefaction wave through piping to core Possible structural damage resulting in failure to maintain core geometry and cooling Provide conditions for structural damage modeling (not part of this research)

4
RELAP5 Two-Fluid Model Conservation of mass Momentum balance

5
**Air Shock Tube Wave Propagation**

5

6
**Qualitative similarity**

Shock wave remains steep Rarefaction wave spreads as it propagates Quantitative similarity Pressure of Gas 2 Analytic MPa RELAP MPa (0.29% error) Shock wave velocity Analytic m/s RELAP m/s (0.24% error) Velocity of Gas 2 Analytic m/s RELAP m/s (1.7% error)

7
**Takeda and Toda Experiment**

8
**RELAP5 Model of Takeda and Toda Experiment**

Water filled vertical pipe under temperature gradient 283.7K at base 437.9 K at top 5.35 cm inner diameter 3.2 m length 99 nodes, each 3.32 cm in length Saturation pressure at top is 6.96 bar Subcooled liquid initially pressurized to 8.55 bar at top Location of experiment pressure transducers (PT) PT 3 at m from break PT 4 at 1.20 m from break PT 5 at 2.20 m from break 1.5 cm diameter junction for break orifice at top of pipe

9
**RELAP5 Model of Takeda and Toda Experiment**

Abrupt area change model employed Ransom Trapp critical flow model used 0.55 ms break delay time to match delay seen in experiment Effect of wall heat transfer examined, but effects proved negligible Due to short duration of transient fluid temperature change is less than 1 K

10
**Liquid is now in a state of**

Fluid discharge through break causes pressure to drop below saturation pressure until nucleation occurs Nucleation of bubbles slows/stops pressure drop and causes flow to choke at reduced soundspeed Liquid is now in a state of Tension Superheat Vapor formation is thermally limited as spinodial limit is approached

11
**Wave Propagation and Reflection**

Initial pressure drop to nucleation pressure initiates propagation of a rarefaction wave Pressure of liquid decreased below saturation Initiates vaporization Waves reflected off solid boundaries in like sense with similar amplitude Waves reflected off constant pressure boundaries in opposite sense with similar amplitude

12
Spatial Convergence 297 node model with nodal length of m compared with 99 node model Shown at PT 5 99 node model is spatially converged

13
Default Simulation PT 4 Test for time step convergence (fast interphase processes) Comparison with experimental data

14
**Default Simulation 3D Plot**

15
**Default Simulation 2D Contours**

Sound speed Pressure

16
**Schematic of Pressure Drop and Rarefaction**

Initial pressure undershoot and void formation Sets pressure for rarefaction wave Rarefaction wave reflects off pipe end and returns to top of pipe More voiding and nonequilibrium effects occur

17
**Reflection at Region of Sound Speed Change**

Sound speed changes at two-phase region (Davis, Princetion Univ Press, 2000) 1500 m/s for single-phase 50 m/s for two-phase Equation to calculate amplitudes AR - amplitude of reflected wave AI - amplitude of incident wave AT - amplitude of transmitted wave cT - transmitted fluid sound speed cI - incident fluid sound speed Wave will reflect in opposite sense with a magnitude similar to the incident wave

18
Default simulation Rarefaction wave interacting with temperature gradient Subsequent voiding occurs Separate two-phase flow region appears Wave becomes trapped Two-phase region expands outward Nonequilibrium effects

19
**Effect of Discharge Coefficient at PT 3**

20
**Interfacial Heat Transfer**

Superheated liquid bubbly flow regime (at break) Energy transfer from liquid to bubble interface Interfacial area concentration, , important

21
**1/10 Bubble Diameter & 0.5 Discharge Coefficient PT 3**

22
**1/10 Bubble Diameter & 0.5 Discharge Coefficient PT 4**

23
**1/10 Bubble Diameter & 0.5 Discharge Coefficient PT 5**

24
Conclusions RELAP5 proved capable of simulating fast transients with depressurizations and acoustic pressure wave propagation RELAP5 simulation of air shock tube successfully validated with an analytic solution RELAP5 simulation of two-phase decompression and wave propagation benchmarked with experimental data Shortcomings in RELAP5 application identified Interfacial area concentration Choked flow model After adjustments the simulation produced better results Cause of dispersion and dissipation of wave identified as it being trapped inside a two-phase region

25
End

26
**Justification for Bubble Diameter**

Bubble growth controlled thermally for duration of the experiment Bubble radius can be calculated using Plesset-Zwick theory with Rayleigh-Plesset equation Bubble radius magnitude less than 2.3 mm bubble radius from RELAP5 Justifies 0.1 multiplication factor for Laplace Length

27
**Effect of Bubble Diameter PT 3**

28
**Effect of Discharge Coefficient at PT 3**

Critical or Choked flow model is important in calculating initial pressure undershoot The RELAP5 Default simulation overpredicts the pressure undershoot Correlation by Alamgir and Lienhard used by RELAP5 for pressure undershoot Valid for pressure drop rates between and Matm/s Pressure drop rate calculated to be Matm/s based on experimental data by Takeda and Toda Subcooled discharge coefficient adjusted to correct for overprediction of pressure undershoot Equivalent to reducing break area Values less than 1.0 recommended for orifices Could be remnants of Mylar paper obstructing break flow

29
**Air Shock Tube RELAP5 model of air shock tube**

Validate use of RELAP5/MOD3.3 to predict single-phase wave propagation Benefit of air shock tube is analytic solution exists Gas 3 initialized at higher pressure than Gas 1 Adiabatic and initially isothermal

30
**Critical Flow Model Comparison of**

Ransom-Trapp Henry-Fauske Ransom-Trapp matches experimental results better and was used

Similar presentations

OK

Flow over an Obstruction MECH 523 Applied Computational Fluid Dynamics Presented by Srinivasan C Rasipuram.

Flow over an Obstruction MECH 523 Applied Computational Fluid Dynamics Presented by Srinivasan C Rasipuram.

© 2018 SlidePlayer.com Inc.

All rights reserved.

Ads by Google

Ppt on cross docking pictures Ppt on dubai in hindi Ppt online open university Ppt on marie curie's discoveries Animated ppt on magnetism definition Ppt on chapter why do we fall ill for class 9 Ppt on natural disasters free download Ppt on time response analysis Liquid crystal on silicon display ppt online Ppt on political parties and electoral process