HYDRODYNAMIC EVOLUTION OF IFE CHAMBERS WITH DIFFERENT PROTECTIVE GASES AND PRE-IGNITION CONDITIONS Zoran Dragojlovic and Farrokh Najmabadi University of.

Slides:



Advertisements
Similar presentations
Heat Transfer to Solids in a Flowing Fluid
Advertisements

Chapter Four Fluid Dynamic
Chapter Four Fluid Dynamic
Lecture 15: Capillary motion
ES 202 Fluid and Thermal Systems Lecture 28: Drag Analysis on Flat Plates and Cross-Flow Cylinders (2/17/2003)
Chapter 7 : Convection – External Flow : Cylinder in cross flow
Thermodynamics April 27, 2015April 27, 2015April 27, 2015.
External Convection: Laminar Flat Plate
Progress Report on SPARTAN Chamber Dynamics Simulation Code Farrokh Najmabadi and Zoran Dragojlovic HAPL Meeting February 5-6, 2004 Georgia Institute of.
Transport phenomena in chemical processes part III Michał Araszkiewicz PhD.
September 24-25, 2003 HAPL meeting, UW, Madison 1 Armor Configuration & Thermal Analysis 1.Parametric analysis in support of system studies 2.Preliminary.
Chapter 2: Overall Heat Transfer Coefficient
Flow over an Obstruction MECH 523 Applied Computational Fluid Dynamics Presented by Srinivasan C Rasipuram.
CHE/ME 109 Heat Transfer in Electronics LECTURE 17 – INTERNAL FORCED CONVECTION FUNDAMENTALS.
April 6-7, 2002 A. R. Raffray, et al., Modeling of Inertial Fusion Chamber 1 Modeling of Inertial Fusion Chamber A. R. Raffray, F. Najmabadi, Z. Dragojlovic,
Engineering H191 - Drafting / CAD The Ohio State University Gateway Engineering Education Coalition Lab 4P. 1Autumn Quarter Transport Phenomena Lab 4.
Thermal Analysis of Helium- Cooled T-tube Divertor S. Shin, S. I. Abdel-Khalik, and M. Yoda ARIES Meeting, Madison (June 14-15, 2005) G. W. Woodruff School.
Preliminary Assessment of Porous Gas-Cooled and Thin- Liquid-Protected Divertors S. I. Abdel-Khalik, S. Shin, and M. Yoda ARIES Meeting, UCSD (March 2004)
EFFECTS OF CHAMBER GEOMETRY AND GAS PROPERTIES ON HYDRODYNAMIC EVOLUTION OF IFE CHAMBERS Zoran Dragojlovic and Farrokh Najmabadi University of California.
IFE Chambers: Modeling and Experiments at UCSD Farrokh Najmabadi 5 th US-Japan Workshop on Laser IFE March 21-23, 2005 General Atomics, San Diego Electronic.
Prediction of Fluid Dynamics in The Inertial Confinement Fusion Chamber by Godunov Solver With Adaptive Grid Refinement Zoran Dragojlovic, Farrokh Najmabadi,
Chamber Dynamic Response Modeling Zoran Dragojlovic.
Progress Report on Chamber Dynamics and Clearing Farrokh Najmabadi, Rene Raffray, Mark S. Tillack, John Pulsifer, Zoran Dragovlovic (UCSD) Ahmed Hassanein.
Nov 13-14, 2001 A. R. Raffray, et al., Progress Report on Chamber Clearing Code Effort 1 Progress Report on Chamber Clearing Code Development Effort A.
California State University, Chico
Introduction to Convection: Flow and Thermal Considerations
Thermal Development of Internal Flows P M V Subbarao Associate Professor Mechanical Engineering Department IIT Delhi Concept for Precise Design ……
Chapter 7 Sections 7.4 through 7.8
In the analysis of a tilting pad thrust bearing, the following dimensions were measured: h1 = 10 mm, h2 = 5mm, L = 10 cm, B = 24 cm The shaft rotates.
Convection Prepared by: Nimesh Gajjar. CONVECTIVE HEAT TRANSFER Convection heat transfer involves fluid motion heat conduction The fluid motion enhances.
Introduction to Convection: Flow and Thermal Considerations
Introduction to COMSOL Travis Campbell Developed for CHE 331 – Fall 2012 Oregon State University School of Chemical, Biological and Environmental Engineering.
FREE CONVECTION Nazaruddin Sinaga Laboratorium Efisiensi dan Konservasi Energi Jurusan Teknik Mesin Universitas Diponegoro.
The Sun Earth Science - Mr. Gallagher. The Sun is the Earth's nearest star. Similar to most typical stars, it is a large ball of hot electrically charged.
Atmospheric pressure and winds
Enhancement of Heat Transfer P M V Subbarao Associate Professor Mechanical Engineering Department IIT Delhi Invention of Compact Heat Transfer Devices……
Anharmonic Effects. Any real crystal resists compression to a smaller volume than its equilibrium value more strongly than expansion to a larger volume.
Status of Target Injector and In-Chamber Tracking Ronald Petzoldt, Dan Goodin, Neil Alexander, Gottfried Besenbruch, Tom Drake, Brian Vermillion, Bob Stemke,
Progress Report on SPARTAN Simulation of IFE Chamber Dynamics Farrokh Najmabadi and Zoran Dragojlovic HAPL Meeting March 3-4, 2005 Naval Research Laboratory.
Chapter 6 Introduction to Forced Convection:
 Heat is measured in Joules or calories.  1 cal = J  Food energy in measured in Calories (with an upper case C)  1 Cal = 1000 cal.
1 Calorimeter Thermal Analysis Revision C November
30 th June 20111Enrico Da Riva, V. Rao Parametric study using Empirical Results June 30 th 2011 Bdg 298 Enrico Da Riva,Vinod Singh Rao CFD GTK.
What set the atmosphere in motion?
Convection: Internal Flow ( )
1 Challenge the future The Lateral Motion of Wafer under the Influence of Thin-film Flow Leilei Hu Solid and Fluid Mechanics
SPARTAN Chamber Dynamics Code Zoran Dragojlovic and Farrokh Najmabadi University of California in San Diego HAPL Meeting, June 20-21, 2005, Lawrence Livermore.
Numerical study of flow instability between two cylinders in 2D case V. V. Denisenko Institute for Aided Design RAS.
Convection in Flat Plate Boundary Layers P M V Subbarao Associate Professor Mechanical Engineering Department IIT Delhi A Universal Similarity Law ……
Temperature Response and Ion Deposition in the 1 mm Tungsten Armor Layer for the 10.5 m HAPL Target Chamber T.A. Heltemes, D.R. Boris and M. Fatenejad,
4th International Conference on Hydrogen Safety, San Francisco, USA, September, J. Yanez, A. Kotchourko, M. Kuznetsov, A. Lelyakin, T. Jordan.
Physics Section 8.3 Apply the properties of flowing fluids The flow of a fluid is laminar if every particle that passes a particular point moves along.
INTRODUCTION TO CONVECTION
1 Linear Wave Equation The maximum values of the transverse speed and transverse acceleration are v y, max =  A a y, max =  2 A The transverse speed.
Sarthit Toolthaisong FREE CONVECTION. Sarthit Toolthaisong 7.2 Features and Parameters of Free Convection 1) Driving Force In general, two conditions.
Lecture 6 The boundary-layer equations
Halliday/Resnick/Walker Fundamentals of Physics
Monday April 26, PHYS , Spring 2004 Dr. Andrew Brandt PHYS 1443 – Section 501 Lecture #24 Monday, April 26, 2004 Dr. Andrew Brandt 1.Fluid.
Simulation of heat load at JHF decay pipe and beam dump KEK Yoshinari Hayato.
Progress Report on SPARTAN Chamber Dynamics Simulation Code Farrokh Najmabadi, Zoran Dragojlovic HAPL Meeting April 8-10, 2003 Sandia National Laboratory,
Chopper Beam Dump Thermal Problem 10/27/20101PX Linac FE Technical Discussions.
Internal Flow: General Considerations. Entrance Conditions Must distinguish between entrance and fully developed regions. Hydrodynamic Effects: Assume.
Chapter 8: Internal Flow
Chamber Dynamic Response Modeling
Anharmonic Effects.
Natural Convection New terms Volumetric thermal expansion coefficient
Anharmonic Effects.
Internal Flow: General Considerations
The sun gives off tremendous amounts of energy
Presentation transcript:

HYDRODYNAMIC EVOLUTION OF IFE CHAMBERS WITH DIFFERENT PROTECTIVE GASES AND PRE-IGNITION CONDITIONS Zoran Dragojlovic and Farrokh Najmabadi University of California in San Diego Twenty-first IEEE/NPSS Symposium on Fusion Engineering 2005

Motivation/Thesis Motivation: –To understand the chamber conditions with different fill gases and initial pressures at 100 ms. The emphasis is on Deuterium and Helium as they will always exist in the chamber. –To explore the impact of gas temperature on target survival. –To explore the deflection of target during injection by velocity drag and pressure gradient. Thesis I: –Xenon was chosen as fill gas because it easily absorbs and re- radiates the energy released by the target. –Deuterium and Helium absorb less energy. They are expected to be “cooler” and thus have less impact on a target.

z r   fill gas IFE Chamber Model SPARTAN numerical algorithm: –Godunov solver of Navier-Stokes equations with state dependent transport properties and radiation heat sink. –Embedded boundary. –Adaptive mesh refinement. Cylindrical Geometry: –Arrays of beam lines around chamber perimeter replaced by a single beam sheet. –A beam line placed on top and bottom. Chamber Initial Conditions: –Chamber state after the target blast and before the impact of the pressure wave with the wall is 1-D. –1-D rad-hydro code BUCKY was used to obtain a matrix of initial conditions for the parametric study. chamber dimensions: radius: 6.5 m height: 13 m beam sheet dimensions: length: 20 m width: 1 m BUCKY initial conditions

Final Chamber Temperature

He Final Temperature Distributions at 100 ms 30 mTorr 50 mTorr DXe Deuterium almost reaches the wall temperature. The difference between the contour lines is 20K. [K] T max 3 mTorr

Final Temperatures of Chamber Gas at 100 ms Base pressure < 50 mTorr Base pressure = 50 mTorr Deuterium at both base pressures has a nearly uniform temperature, within K from the equilibrium with the wall. Average temperature of the Helium is within 200 K from the wall temperature, only the central hot region stands out. Even at 3 mTorr, Xenon is considerably hot (T max ~ 3000 K). Reducing the base pressure from 50 mTorr (as shown on the right) to 3 mTorr (as shown on the left) does not help to bring Xe to the thermal equilibrium with the wall. 3 mTorr 30 mTorr

Thermal Regimes in The Chamber The initial temperatures are different because the initial conditions are taken at different times. Heating due to shockwave compression and subsequent cooling by radiation govern the chamber temperatures in the first millisecond. The exponentially decaying parts of the curves correspond to “free cooling”. compressive heating and cooling by radiation “free cooling” 1 st bullet 2 nd and 3 rd bullet = K

Final Chamber Velocities

Initial Velocities from BUCKY Code Base pressure < 50 mTorrBase pressure 50 mTorr Initially, Deuterium has a much higher velocity than Xenon, due to its lower mass. At 50 mTorr, the peak velocity of Xenon is 2.6 km/s, while the peak velocity of Deuterium is 60 km/s.

He Final Velocities at 100 ms 30 mTorr 50 mTorr D Xe Even though the initial velocity of Deuterium was much higher than Xenon, final velocity of Deuterium is similar to that of Xenon, due to the lower final temperature of Deuterium. Xenon at 50 mTorr shows turbulence – note the “smoky” features. The Reynolds number for this case is 8,600. For all the other cases, the Re ~ 100. [m/s] 3 mTorr

Impact on the Target

Acceleration of Target Due to Drag Force at 100 ms Base pressure < 50 mTorrBase pressure = 50 mTorr Accelerations are based on velocity field in the chamber (excluding beam lines), gas viscosity, target diameter of 4 mm and target mass of 4.8 milligrams. Drag force depends on gas velocity and viscosity. Acceleration of target by Deuterium is smaller than that of Xenon at the same base pressure because the viscosity of Xenon is 5 times higher than viscosity of Deuterium. At 3 mTorr, Xenon exerts a drag force on the target, comparable to D and He at ten times higher base pressures. deflects target by 2mm (injection speed = 500 m/s) 3 mTorr mTorr

Chamber Gas Pressures at 100 ms Base pressure < 50 mTorrBase pressure = 50 mTorr Only Deuterium returns to within several pascals from the base pressure, 100 ms after the target ignition. Chamber gas pressures of Deuterium and Helium gas are nearly uniform (min ≈ ave ≈ max), while Xenon at base pressure 50 mTorr is highly non-uniform (max/min ≈ 3). 3 mTorr 50 mTorr 30 mTorr

Acceleration of Target Due to Pressure Gradients at 100 ms Base pressure < 50 mTorrBase pressure 50 mTorr Accelerations are based on the pressure gradients in the chamber (excluding beam lines), target diameter of 4 mm and target mass of 4.8 milligrams. The acceleration of target due to pressure gradients is negligible compared to the acceleration caused by drag force. 3 mTorr 30 mTorr

Conclusions Deuterium and Helium have low impact on the target, at base pressures in the range of mTorr. –Deuterium cools down to the wall temperature within the 100 ms. Helium remains slightly hotter in the center of the chamber but approaches the equilibrium with the wall, on the average. –The flow of D and He is laminar and does not significantly deflect the target from its path. Xenon has a significant impact on the target even at base pressures as low as 3 mTorr. –The temperature of Xenon is above the specs for target survival at 100 ms past the target blast. –The drag force of Xenon acting on the target is comparable to Deuterium and Helium at ten times higher base pressure.