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1 On the Calculation of Magnetic Helicity of a Solar Active Region and a Cylindrical Flux Rope Qiang Hu, G. M. Webb, B. Dasgupta CSPAR, University of Alabama in Huntsville, USA J. Qiu Montana State University, USA qh0001@uah.edu
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2 Acknowledgement NASA grants NNG04GF47G, NNG06GD41G, NNX07AO73G, and NNX08AH46G (data provided by various NASA/ESA missions, and ground facilities; images credit: mostly NASA/ESA unless where indicated) Debi P. Choudhary B. Dasgupta Charlie Farrugia G.A. Gary Yang Liu Dana Longcope Jiong Qiu D. Shaikh R. Skoug C. W. Smith/N.F. Ness W.-L. Teh Bengt U. Ö. Sonnerup Vasyl Yurchyshyn Gary Zank Collaborators:
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3 Overview Helical Structures: Interplanetary Coronal Mass Ejections –In-situ detection and magnetic flux rope model –GS technique and its applications MDR-based coronal magnetic field extrapolation Homotopy formula for magnetic vector potential Summary and Outlook
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4 Coronal Mass Ejection (CME) (Moore et al. 2007) Simultaneous multi-point in-situ measurements of an Interplanetary CME (ICME) structure ( Adapted from STEREO website, http://sprg.ssl.berkeley.edu/impact/instruments_boom.html )
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5 in-situ spacecraft data Cylindrical flux-rope model fit (Burlaga, 1995; Lepping et al., 1990, etc.) In-situ Detection and Modeling
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6 x: projected s/c path GS Reconstruction method: derive the axis orientation (z) and the cross section of locally 2 ½ D structure from in-situ single spacecraft measurements (e.g., Hu and Sonnerup 2002). Main features: - 2 ½ D - self-consistent - non-force free - flux rope boundary definition - multispacecraft actual result:
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7 Output: 1.Field configuration 2.Spatial config. 3.Electric Current. 4.Plasma pressure p(A). 5.Magnetic Flux : - axial (toroidal) flux t = B z x y - poloidal flux p =|A b - A m |*L 6.Relative Helicity: K rel =2L A’· B t dxdy A’=B z z ^ Reconstruction of ICME Flux Ropes ( 1D 2D) Ab Ab AmAm ACE Halloween event (Hu et al. 2005)
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8 z =(0.057, 0.98, -0.18) ± (0.08, 0.01, 0.03) RTN July 11, 1998 [Hu et al, 2004]
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9 Field line twist, Flux rope 1 Flux rope 2 Pink 4.2 2 /AU 4.7 2 /AU Blue 1.9 2 /AU 1.9 2 /AU View towards Sun: 2 ~ 10 25 -10 26 Wb 2 z
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10 CMEICME Sun at Earth propagation Sun-Earth Connection 1.Orientation of flux rope CME/ICME ( Yurchyshyn et al. 2007 ) 2.Quantitative comparison of magnetic flux ( Qiu et al. 2007 )
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11 poloidal or azimuthal magnetic flux P : the amount of twist along the field lines The helical structure, in-situ formed flux rope, results from magnetic reconnection. toroidal or axial magnetic flux t Longcope et al (2007) ribbons poloidal flux P reconnection flux r reconnection 3D view (Gosling et al. 1995) (Moore et al. 2007) Credit: ESA reconnection
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12 Comparison of CME and ICME fluxes ( independently measured for 9 events ; Qiu et al., 2007 ): - flare-associated CMEs and flux-rope ICMEs with one-to-one correspondence; - reasonable flux-rope solutions satisfying diagnostic measures; - an effective length L=1 AU (uncertainty range 0.5-2 AU). GS method Leamon et al. 04 Lynch et al. 05 P ~ r
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13 One existing simple model, variational principle of minimum energy (e.g., Taylor, 1974; Freidberg, 1987): However, Amari and Luciani (2000), among others, showed by 3D numerical simulation that in certain solar physics situation, …, the final “relaxed state is far from the constant- linear force-free field that would be predicted by Taylor’s conjecture” …, and suggested to derive alternative variational problem. Linear force-free field (LFFF, const) Or, Nonlinear FFF ( varies) Coronal Magnetic Field Extrapolation ( 2D 3D)
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14 An alternative... Simple Examples: Current distribution in a circuit Total ohmic dissipation is minimum Velocity profile of a viscous liquid flowing through a duct Total viscous dissipation is minimum Principle of Minimum Dissipation Rate (MDR): the energy dissipation rate is minimum. ) (Montgomery and Phillips,1988; Dasgupta et al. 1998; Bhattacharyya and Janaki, 2004) (Several extended variational principles of minimum energy ( Mahajan 2008; Turner 1986 ) yield solutions that are subsets to the above) (Several extended variational principles of minimum energy ( Mahajan 2008; Turner 1986 ) yield solutions that are subsets to the above)
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15 For an open system with flow, the MDR theory yields (Bhattacharyya et al. 2007; Hu et al., 2007; Hu and Dasgupta, 2008, Sol. Phys.) Take an extra curl to eliminate the undetermined potential field , one obtains New Approach
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16 (5) (7) (8) Equations (5),(7) and (8) form a 3 rd order system. It is guaranteed invertible to yield the boundary conditions for each B i, given measurements of B at bottom boundary, provided the parameters, 1, 2 and 3 are distinct.
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17 Above equations provide the boundary conditions (normal components only at z=0) for each LFFF B i, given B at certain heights, which then can be solved by an LFFF solver based on FFT (e.g, Alissandrakis, 1981). One parameter, 2 has to be set to 0. The parameters, 1 and 3, are determined by optimizing the agreement between calculated (b) and measured transverse magnetic field at z=0, by minimizing Measurement error Measurement error + Computational error <0.5?
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18 Reduced approach: choose B 2 =cB’, proportional to a reference field, B’= A’, and B’ n =B n, such that the relative helicity is A BdV- A’ B’dV, with A=B 1 / 1 +B 3 / 3 +cA’. B’=0, B z ’=B z, at z=0 Only one layer of vector magnetogram is needed. And the relative helicity of a solar active region can be calculated. (As a special case, B 2 =0, in Hu and Dasgupta, 2006)
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19 Iterative reduced approach: transverse magnetic field vectors at z=0 (E n =0.32): k=0 Reduced approach: Obtain E (k) and If E (k) < End Y N k=k+1 n n k>k max Y
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20 Test Case of Numerical Simulation Data ( Hu et al. 2008, ApJ ) (a)“exact” solution (Courtesy of Prof. J. Buechner) (b) our extrapolation (128 128 63)
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21 Transverse magnetic field vectors at z=0 ( E n =0.30 ): Figures of merit (Hu et al., 2008, ApJ): Energy ratios
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22 Integrated current densities along field lines: (a) exact (b) extrapolated J_para J_perp 0
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23 E/E p_pre=1.26 E/E p_post=1.30 (Data courtesy of M. DeRosa, Schrijver et al. 2008; Hinode is a Japanese mission developed and launched by ISAS/JAXA, with NAOJ as domestic partner and NASA and STFC (UK) as international partners. It is operated by these agencies in co-operation with ESA and NSC (Norway).
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24 Main Features More general non-force free (non- vanishing currents); Better energy estimate Fast and easy (FFT-based); Make it much less demanding for computing resources Applicable to one single-layer measurement ( Hu et al. 2008, 2009 ) Applicable to flow
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25 Homotopy formula for vector magnetic potential (based on ):
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26 (Berger, M.) “In topology, two continuous functions …topologycontinuousfunctions if one can be "continuously deformed" into the other, such a deformation being called a homotopy between the two functions.” -- Wikipedia
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27 Relative magnetic helicity via homotopy formula: B z (x,y) r Kr/AU: 3.5 x 10 23 Wb 2 Kr/AU ( Hu and Dasgupta, 2005 ): 3.4 x 10 23 Wb 2
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28 Relative magnetic helicity via homotopy formula: B in a 3D volume r (e.g., see Longcope & Malanushenko, 2008)
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29 Multi-pole expansion of a potential field: For each 2 k -th pole, B (k), (via a modified homotopy formula) Dipole: Related to spherical harmonic expansion, for example. For MDR-based extrapolation: A simplified vector potential for a potential field?
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30 Outlook Validate and apply the algorithm for one-layer vector magnetograms Validate the theory – proof of MDR by numerical simulations Global non-force free extrapolation Stay tuned!
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32 MHD states:
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33 Dec. 12-13 2006 Flare and CME (Schrijver et al. 2008) (KOSOVICHEV & SEKII, 2007) (SOHO LASCO CME CATALOG http://cdaw.gsfc.nasa.gov/CME_list/)
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34 Reduced approach: transverse magnetic field vectors at z=0 (E n =0.7-0.9): Measured Computed (Data courtesy of M. DeRosa, Schrijver et al. 2008; Hinode is a Japanese mission developed and launched by ISAS/JAXA, with NAOJ as domestic partner and NASA and STFC (UK) as international partners. It is operated by these agencies in co-operation with ESA and NSC (Norway).
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35 En=0.28 Post-flare case:
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36 En( 1, 3 ):
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38 Principle of minimum dissipation rate (MDR) In an irreversible process a system spontaneously evolves to states in which the energy dissipation rate is minimum. A different variational principle Suggests a minimizer for our problem 1.R. Bhattacharyya and M. S. Janaki,Phys. Plasmas 11, 615 (2004). 2.D. Montgomery and L. Phillips, Phys. Rev. A 38, 2953, (1988). 3.B. Dasgupta, P. Dasgupta, M. S. Janaki, T. Watanabe and T. Sato, Phys. Rev. Letts, 81, 3144, (1998)
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39 L Onsager, Phys. Rev, 37, 405 (1931) I. Prigogine, Thermodynamics of Irreversible Processes, Wiley (1955 ) ------------------------------------------------------------------------------------------------------ A theorem from irreversible thermodynamics: Principle of Minimum Entropy Production “The steady state of an irreversible process, i.e., the state in which thermodynamics variables are independent of time, is characterized by a minimum value of the rate of Entropy Production” Rate of Minimum Entropy Production is equivalent to Rate of Minimum Dissipation of Energy in most cases.
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40 Numerical simulation (Shaikh et al., 2007; NG21A-0206 ) showed the evolution of the decay rates associated with the turbulent relaxation, viz, Magnetic Helicity K M, Magnetic Energy W M and the Dissipation Rate R. K M = W M = R=
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41 The generalized helicity dissipation rate is time-invariant. Formulation of the variational problem (for an open system with external drive, or helicity injection) constraint ( = i, e) From the MDR principle, the minimizer is the total energy dissipation rate variational problem
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42 Euler-Lagrange equations Eliminating vorticity in favor of the magnetic field
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43 Summary of Procedures magnetohydrodynamic
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44 Analytic Test Case: non-force free active region model given by Low (1992) Top View:
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45 A real case: Active Region (AR)8210 (preliminary) ( Choudhary et al. 2001 ) Imaging Vector Magnetograph (IVM) at Mees Solar Observatory (courtesy of M. Georgoulis)
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46 E n distribution:
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47 One-fluid Magnetohydrostatic Theory –2 ½ D: B z 0 –Co-moving frame: DeHoffmann-Teller (HT) frame –No inertia force Grad-Shafranov (GS) Equation (A=A z ): P t (A)=p(A)+B z (A)/2 0 A B t = 0 2 GS Reconstruction
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48 GS Reconstruction Technique 1.Find z by the requirement that P t (A) be single-valued 2.Transform time to spatial dimensions via V HT, and calculate A(x,0), 3.Calculate P t (x,0) directly from measurements. 4.Fit P t (x,0)/B z (x,0) vs. A(x,0) by a function, P t (A)/B z (A). A boundary, A=A b, is chosen. 5.Computing A(x,y) by utilizing A(x,0), B x (x,0), and GS equation. ^ x: projected s/c path AmAm o:inbound *:outbound
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49 Finding z axis by minimizing residue of P t (A): Residue=[∑ i (P t,i – P t,i ) 2 ] / |max(P t )-min(P t )| A(x,0) P t (x,0) Pt(A)Pt(A) o: 1st half *: 2nd half i=1…m 1212 1st2nd Enumerating all possible directions in space to find the optimal z axis for which the associated Residue is a minimum. A residue map is constructed to show the uniqueness of the solution with uncertainty estimate.
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50 GS Solver:
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51 Multispacecraft Test of GS Method Cluster FTEs (from Sonnerup et al., 2004; see also Hasegawa et al. 2004, 2005, 2006)
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52 Introduction Grad-Shafranov (GS) equation: p=j B in 2D GS technique: solve GS equation using in-situ data, 1D 2D (e.g., Sonnerup and Guo, 1996; Hau and Sonnerup, 1999; Hu and Sonnerup, 2000, 2001, 2002, 2003; Sonnerup et al. 2006 )
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53 Small-scale flux ropes in the solar wind ( Hu and Sonnerup, 2001 )
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54 Features of the GS Reconstruction Technique: -Fully 2 ½ D solution (less fitting) -Self-consistent theoretical modeling; boundary definition (less subjective) -Utilization of simultaneous magnetic and plasma measurements; Non-force free -Adapted to a fully multispacecraft technique (Hasegawa et al. [2004]) Limitations (diagnostic measures): -2D, uncertainty in z (the quality of P t (A) fitting, R f ) 2D P t (A), P t (A) 2D -Time stationary (quality of the frame of reference) -Static (evaluating the residual plasma flow) -Numerical errors limit the extent in y direction (rule of thumb: |y| |x|, y« x) ?
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55 : Wind data oo : Predicted ACE-Wind comparison
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56 July 11 1998 event -Apparent magnetic signatures of multiple structures denoted by 1, and 2. - GS reconstruction is applied to the larger interval (solid vertical lines) and subintervals 1, and 2. 12
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57 Case A ’=(-2º,-90º) Case B ’=(2º,-90º) r r Z Z o : ’ x : Z’ The exact orientation =(0º,-90º); in both cases the results are much better than cylindrical models ( Riley et al., 2004 ).
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58 ACE-Ulysses comparison (Du et al., 2007) Fluxes at ACE (length D= *1AU): t Wb P =44 TWb Helicity : -1.4* *10 23 Wb^2 At Ulysses (D=5.4AU): t Wb P =14 TWb Helicity : -3.7* *10 21 Wb^2
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59 2D 3D? May 22-23, 2007 Event (courtesy of C. Farrugia)
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60 ( Yurchyshyn et al. 2005, 2007 ) at Earth Prediction? connection Multi-wavelength, multi-instrument data analysis & modeling
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61 CME x Connection Between MC flux, and Flux due to Magnetic Reconnection in Low Corona (Qiu et al. 2007) flare ribbons Flare loops reconnection site (adapted from Forbes & Acton, 1996) MC Flux : MC : mostly poloidal component P (measured in-situ at 1 AU) At sun: MC = pre-existing flux if any + reconnection flux r P r
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62 GS Reconstruction of Locally Toroidal Structure ( Riley et al., 2004) GS result
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63 ~ 64% agreement rate ( Yurchyshyn et al. 2007)
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64 (Gosling et al. 1995) 3D view
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65 CME: the flux rope set free Different scenarios (Gosling et al. 1995):
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66 reconnection rate (general) dA C BCBC BRBR dA R reconnection V in “measure” reconnection rate v v flare at an earlier time flare at a later time MDI magnetogram dA R observation: flares and magnetic fields model : Forbes & Priest 1984
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67 The flare-CME connection: some models loss of equilibrium (Forbes-Priest-Lin) CME front filament flare magnetic breakout (Antiochos et al. 1999) overlying flux post-flare loop reconnection emerging flux Does the CME know the flare?
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68 Forbes (2000) pre-existing flux rope (Chen 1989, Low 1996, Forbes- Priest-Lin, Fan-Gibson) What do we see as a magnetic flux rope? SXR sigmoid prominence (HAO) SXT/Yohkoh Gibson, 2005 Harvey Prize Lecture
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