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Pl;Oe Flow Through a Solenoid of Finite Length Experimental Studies in Pl;oe Flow Through a Solenoid of Finite Length T. Maxworthy - - ___- I -.- I !;$$) - I.*. ! JET PROPULSION LABORATORY '\ CALIFORNIA INSTITUTE OF TECHNOLOGY \, , \ \ :< :< :1 PASADENA, CALIFORNIA 1. *f 'v: December 15, 1967 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Technical Report 32-7798 Experimental Studies in Magneto-Fluid Dynamics: Pipe Flow Through a Solenoid of Finite Length T. Maxworthy Approved by: A. L. Kistler, Manager Fluid Physics Section JET PROPULSION LABORATORY CALIFORNIA INSTITUTE OF TECHNOLOGY PASADENA, CALIFORNIA December 15, 1967 TECHNICAL REPORT 32-I 7 98 Copyright 0 1967 Jet Propulsion Laboratory California Institute of Technology Prepared Under Contract No. NAS 7-100 National Aeronautics & Space Administration 'PAGE BLANK NOT FILMED. Contents 1. Introduction ................ 1 II . Fluid Dynamical Design Parameters .......... 2 111. Design and Description of the Flow System ........ 2 A . Magnet and Nozzle Design ........... 3 B . Wide-Angle Diffuser ............. 3 C . Test Section. Probe. and Model Traverse ........ 3 IV. Instrumentation ............... 6 A . Pressure-Measuring Devices ........... 6 B . Magnetic Field .............. 7 C. FIowRate ............... 8 D. Applied Magnetic Field ............ 8 V . Results and Discussion .............. 8 A . Results and Deductions from Measurements of Static Pressure ................ 8 B . Deductions from Measurements of Total Pressure .....14 C . Velocity Measurements ............15 D. Flow Characteristics with Modified Magnetic Field .....15 VI . Conclusions ................ 16 Appendix . Pressure Distribution Measurements ........17 References .................. 17 Table 1 . Characteristic parameters ............. 2 ... JPl TECHNICAL REPORT 32-1 198 111 Contents (contd 1 Figures 1. Photograph of the liquid sodium tunnel, with test section and traversing mechanism in the foreground . 4 2. (a) Diagrammaticview of the liquid sodium flow loop; (b) cross-section through the test section and probe traversing mechanism . 5 3. (a) interaction between the magnetic field of a solenoid and the flow of an initially parallel stream of conducting fluid; (b) view showing how the interaction between fluid and magnetic field can be modified by shaping of the inlet nozzle . 6 4. Diagrammatic view of force balance on particles close to a pressure measuring orifice . 7 5. Longitudinal static pressure profiles at various radial locations and flow rates (B, = 0.70 Wb/m2) . 9 6. Radial static pressure profiles at various axial stations and flow rates (B, = 0.70 Wb/mz) . 10 7. Distribution of current density je in the test section forN=12.1 . 11 8. Variation of current density distribution with N; location of maximum je . 12 9. Variation of static pressure on centerline with axial distance . 12 10. Variation in centerline magnetic field perturbation with axial distance from exit of magnet . 13 1 1. Variation of exponent m with N . 13 12. Location of the cross-section at which the current density changes sign . 13 13. Variation of total pressure in test section (x = 0) at fixed magnetic field strength and variable flow rate . 15 14. Velocity calibration curves . 15 iv JPL TECHNICAL REPORT 32-1 198 Contents (contd 1 Figures (contd) 15. Velocity profiles: (a) velocity profiles at various axial locations for N = 12.1; (b) normalized velocity profiles for B, = 0.70 Wb/m2, various N at the center of the magnet, x/a = 0 ...............16 16. Longitudinal static pressure profile in magnet with no shaping of the inlet flow B, = 0.70 Wb/m2, N = 12.1 ........ 16 A-1. 1 - CP, vs N sphere, for test sphere located at several axial positions within tunnel ............ 17 JPL TECHNICAL REPORT 32- I 198 V Abstract A liquid sodium tunnel has been designed and built to study aligned fields, magneto-fluid-dynamic (MFD) flows. Its major features and the nature of the flow in the test section are described. In particular, it is found that an exit disturbance, created as the liquid conductor leaves the region of magnetic field, can propagate into the test section and affect the flow there. However, only under the most adverse conditions, i.e., very high magnetic fields and low flow velocities, does this impair the usefulness of the tunnel as a device for the accurate measurement of MFD flows. vi JPL TECHNICAL REPORT 32-7798 Experimental Studies in Magneto-Fluid Dynamics: Pipe Flow Through a Solenoid of Finite Length’ 1. Introduction stantiated by accurate experimental observation. These are described as follows: In the summer of 1961, an ambitious program was begun, aimed at attempting to understand the physical (1) The existence of the “precursive wake,” a region of processes underlying the motions created by a conducting vorticity and current density generated by the prop- fluid as it flowed around an object placed in an aligned agation of disturbances ahead of a body when it is magnetic field.2 Once these processes had been exposed, placed in an aligned magnetic field. it was hoped that they would be amenable to some rea- sonable theoretical treatment which would eventually (2) The nature of the rearward or conventional wake point the way to general principles applicable in a variety behind a body. of magneto-fluid-dynamic problems. The completion of (3) The changes in separation phenomena. this program has yet to be realized, so we confine our- selves in this report and in those which follow, to a descrip- (4) The existence of magneto-fluid-dynamic boundary tion of the facility used in this experimental study, and of layers, the interaction between the magnetic field the flow created in the test section of the device. This is and a flow field distorted by viscous boundary layer followed by a discussion of measurements of (1) the drag displacement effects or by body interactions. force on spheres and disks (Refs. 1,2) and (2) the pressure (5) The changes in drag and lift coefficients due to mag- distribution around a sphere placed in such a flow (Ref. 3). netic interactions. When the project was initiated, the subject was strewn (6) The properties of magneto-turbulence. with hypotheses and predictions that still had to be sub- We wished to study these interactions in a logical way and make accurate measurements. As will be seen, some ‘Subtitled “Description and Flow Characteristics of the JPL Liquid Sodium Tunnel.” of these questions have been satisfactorily answered, while ‘At upstream infinity, flow and magnetic field are parallel. others are still not well understood. JPL TECHNICAL REPORT 32- I 7 98 1 Production of such effects requires that the flowing the tunnel is suited to the measurement of aerodynamic fluid be a good electrical conductor. Most fluids can either flows. be discarded because of their inaccurately known prop- erties (i.e., plasmas) or because of their weak interaction II. Fluid Dynamical Design Parameters with a magnetic field under practically realizable condi- tions (i.e., mercury, ionic solutions). Liquid sodium is the With the addition of two extra quantities to the equa- outstanding exception. It is inexpensive, the interactions tions of fluid motion, viz., an electrical conductivity and are substantial, and a large body of technical information a magnetic field, we now have three independent non- exists concerning its properties and methods of control. dimensional parameters available to characterize the sys- Extensive work, by nuclear engineers, on the use of liquid tem. Six possible parameters are shown in Table 1, together sodium as a heat-transfer medium, means that it was not with their physical interpretation and typical values for necessary to embark upon an extensive hardware develop- sodium and mercury. Rationalized M.K.S.Q. (meters, kilo- ment program. The system was, therefore, designed to grams, seconds, charge) units are used throughout. It is take the fullest advantage of this knowledge as embodied quite apparent that sodium is superior in all respects to in Ref. 4. mercury as a working fluid, unless a mercury system can be made to give accurate answers at very low velocities It is also desirable, in a report such as this, to show to (- 0.01 m/s) and very high magnetic fields (1.2 Wb/m2). what extent the original design has fulfilled its expecta- In this table, d and U, are the body dimension and fluid tions. Included are sections devoted to the measurements velocity, and p, v, and p are the fluid density, kinematic performed in the tunnel using the simplest of the instru- viscosity, electricaI conductivity and permeabiiity; B, is mentation, and the Pitot-static pressure probe. From these the applied magnetic flux density. measurements we can find how the velocity and pressure fields are distorted by the presence of the MFD inter- action. By making suitable assumptions, it is also possible 111. Design and Description of the Flow System to infer the distortions of the applied magnetic field which Two major criteria must be satisfied by our system: the can later be checked against magnetometer measurements first requires that we have a vorticity-free, current-free and the validity of the assumptions verified. An Appendix flow of known steady temperature and velocity in the test on pressure distribution measurements around a sphere section; the second requires that the sodium system be as placed at various axial locations is included to show how safe as possible. Special handling problems must be solved Table 1. Characteristic parametersa Parameter Sodium at 1 5OoC Mercury 1 ~ ~ ~ 6; 6; d - magnetic force - Haa Interaction parometer
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