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Figure 3: Examples of agreement of reconnected flux with minus the accumulation integral of the outof-plane electric field at the origin for fine and coarse mesh. (For the fine mesh the two plots are exactly superimposed and so are indistinguishable.) Flux across the vertical axis represents the portion of field lines that have not reconnected. We obtained similar excellent agreement in all our simulations. Figure 4: Snapshots of magnetic field lines. The reconnected flux is proportional to (the change in) the number of field lines through the horizontal axis of symmetry, and the unreconnected flux is proportional to the number of field lines through the vertical axis of symmetry. 20
19th Annual Conference Part Eight Biological Science
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Space Grant Consortium wisconsin UN
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THE CASSINI ENCOUNTER WITH THE GEM
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Th he proceedinngs of our 199th Ann
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Wisconsin Space Grant Consortium Un
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Part 3: NASA Reduced Gravity Progra
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EAA Women Soar - You Soar, Lee Siud
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Elijah High Altitude Balloon Projec
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Our experience with the HALO II lau
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which had been a problem in the pas
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Figure 6: 3-D GPS Generated Track o
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Results The seeds tested in the lab
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hour as we assumed the flight in th
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Experimental Results There are two
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A series of tests were done in a co
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380 360 340 320 23.3 Temp. (Celsius
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First Place, Non-Engineering: Schmi
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of the basis for fin designs came f
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ejection charge from the motor fire
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using rip-stop nylon cloth. To atta
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Post-flight recovery. A field searc
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Thus, it is believed that the main
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[2] Public Missiles Ltd. Frequently
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Design Features The chief requireme
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The joint between the dart and the
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Area dramatically influenced by flo
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Altitude [ft] 6000 5000 4000 3000 2
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though a strong crosswind was prese
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Our Design Our rocket uses the basi
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e easily recovered. Bong recreation
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Performance Characteristics of Pred
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Background and Context: Student Roc
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The Rocky Mountain Miners’ compet
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19th Annual Conference Part Three N
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The angle of repose of a granular m
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Experiment Design The experiment co
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on the ground and in the Weightless
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measurements for the 1 − g data.
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[ImageJ, 2008] Image Analysis Softw
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Dynamics Characterization of the El
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Figure 1 - A calibration equation f
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Wire A secondary investigation into
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[1] Taminger, K. M. B.; and Hafley,
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Introduction The analysis of wake v
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Figure 2: Screen I mage o f G UI. T
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References ¹ Burnham, D.C., and Ha
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Validation of Novel Rigid Body Fric
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forces is implemented in the popula
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Figure 2. CAD representation of a t
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Results Figure 5. Assembled hydraul
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References Anitescu, M. (2006). "Op
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Multi-stage Joule-Thomson cycles ar
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significant change in total compres
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The enthalpy (h3) of the 2 nd stage
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UA m� ⎛ ε −1 ⎞ ( c nd c st
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educed, the temperature range that
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7. Lemmon, E. W.; Huber, M. L.; McL
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Throughout each of the run cycles,
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and heater adjusted to accommodate
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Phaeton Mast Dynamics Mechanical Sy
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exposure to the FEMAP with NASTRAN
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The irregularity in the plots above
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inversion of a particular matrix, t
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clarified. Additionally, the PMD ki
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A. Abstract For hardware to be flig
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should be performed at the JWST obs
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B. Attenuation and Uncertainty Shoc
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Detector Array and ROIC SCA Mount L
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Detector Shock Environment The leve
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Orbiter (MRO), Moon Mineralogy Mapp
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4. NASA JPL. MIRI FOCAL PLANE SYSTE
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Is Lake Superior a significant sour
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each grid cell at daily resolution.
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Figure 3. (a) Seasonal cycle of lak
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Figure 5. Model pCO2 at the surface
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Marshall, J., A. Adcroft, C. Hill,
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numerical weather prediction (NWP)
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High Resolution Radiometer (AVHRR)
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On the morning of 26 May 2008, ther
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References Behnke, C., 2005: Synopt
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Figure 3 Figure 3 contains base ref
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Page 179 and 180: Fig. 3.— Cartoon Image of SN blas
Page 181 and 182: Fig. 4.— Light curve of SN 2008bo
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Page 190: and then can spiral in to the black
Page 195 and 196: Understanding the Evolution of Supe
Page 197 and 198: Radio  measurements  of  supe
Page 199 and 200: In the equations on the p
Page 201 and 202: SN 2008ax in NGC 4490 SN2008ax is a
Page 203: References Chevalier, R. A., “Int
Page 207 and 208: Computational Fluid Dynamical Model
Page 209 and 210: context of the k − ɛ model invol
Page 211 and 212: Figure 3: Experimental results (•
Page 213 and 214: direction results in the terminal s
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Page 218 and 219: concentrated our effort specificall
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Page 222 and 223: Properties of the GEM problem Recon
Page 224 and 225: Figure 1: Increase in reconnection
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Page 231 and 232: Experimental Procedure The left han
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Page 240 and 241: group started in 1997 with the goal
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Page 246 and 247: explain t his t rend. F rom t alkin
Page 248 and 249: Research. Washington, DC: Pan Ameri
Page 250 and 251: Our team has two goals: 1. To put S
Page 252 and 253: fluctuating humidity, drying winds,
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Page 265 and 266: Abstract Toxic Offgassing Analysis
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Page 269 and 270: Tables 4 and 5 show offgassing comp
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Figure 3: Current versus voltage da
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Abstract New Initiatives in the Pro
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was noticed above the gel. A discol
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delicate structures (hairs). N o fu
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and A. Y. Rozanov, Eds., SPIE, Vol.
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Combining Writing Across the Curric
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But the study also reported a consi
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Educators’ Aerospace Workshop for
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2008-2009 Evaluation Educators’ A
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Some comments from participants 200
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The cost of a one credit graduate c
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EAA WOMEN SOAR - YOU SOAR Dr. Lee J
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� Incorporated the technology res
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Evaluation Results: At the conclusi
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Educational Standards: The National
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curriculum development, to provide
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and applications of GIS technology
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• A significant new outcome for t
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The design of this project and appl
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Activities at the workshop involved
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to give our students a series of PR
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In the past we have not focused on
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Providing High School Students with
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that th e current generations of s
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instruction a s pa rt o f t heir ow
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Wisconsin Space Grant Consortium &
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11:45-1:00 pm Lunch *** Concurrent
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Moderator: David B lock, A ssociate
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Second Place, E ngineering, Drew an
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Wisconsin Space Grant Consortium
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