Space Grant Consortium - University of Wisconsin - Green Bay

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References ¹ Burnham, D.C., and Hallock, J.N., “Chicago Monostatic Acoustic Vortex Sensing System,” Report No. DOT-TSC- FAA-79-103. IV, July 1982, 206 pp. ² Lamb, H., Hydrodynamics, 6 th Ed., Cambridge University Press, 1932, 738 pp. ³ Proctor, F.H., “Interaction of Aircraft Wakes from Laterally Spaced Aircraft,” 47 th Aerospace Sciences Meeting & Exhibit, 5-8 January 2009, AIAA-2009-0343. (2005, Jan. 1). Monitoring Wake Vortices for More Efficient Airports. Originating Technology/ NASA Contribution - Transportation, 16-17. Retrieved July 29, 2009, from http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20060022051_2006145875.pdf 14
Appendix A Variables radii large at n circulatio vortex velocity ngential vortex ta maximum velocity l tangentia of profile radial ) ( velocity gential vortex tan maximum) is V (Where radius core vortex center vortex from distance radial vortices rotating - co between distance separation initial ingspan aircraft w max 0 = Γ = = = = = = = ∞ V r V V r r b B c Burnham-Hallock Model )} /( ){ 2 / ( ) ( 2 2 r r r r V c + Γ = ∞ π Lamb-Oseen Model ]} ) / ( 2527 . 1 exp[ 1 ){ 2 / ( ) ( 2 c r r r V − − Γ = ∞ π TASS Initial Vortex Model c c c c r r r r B r r V r r B r r V 4 . 1 for ]} ) / ( 2527 . 1 exp[ 1 ]}{ ) / 4 . 1 ( 10 exp[ 1 { 0939 . 1 * ) 2 / ( ) ( 4 . 1 for ]} ) / ( 10 exp[ 1 ){ 2 / ( ) ( 2 75 . 0 75 . 0 < − − − − Γ = ≥ − − Γ = ∞ ∞ π π 15
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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
Page 47: [2] Public Missiles Ltd. Frequently
Page 50 and 51: Design Features The chief requireme
Page 52 and 53: The joint between the dart and the
Page 54 and 55: Area dramatically influenced by flo
Page 56 and 57: Altitude [ft] 6000 5000 4000 3000 2
Page 58 and 59: though a strong crosswind was prese
Page 60 and 61: Our Design Our rocket uses the basi
Page 62 and 63: e easily recovered. Bong recreation
Page 64 and 65: Performance Characteristics of Pred
Page 67 and 68: Background and Context: Student Roc
Page 69 and 70: The Rocky Mountain Miners’ compet
Page 71: 19th Annual Conference Part Three N
Page 74 and 75: The angle of repose of a granular m
Page 76 and 77: Experiment Design The experiment co
Page 78 and 79: on the ground and in the Weightless
Page 80 and 81: measurements for the 1 − g data.
Page 82 and 83: [ImageJ, 2008] Image Analysis Softw
Page 85 and 86: Dynamics Characterization of the El
Page 87 and 88: Figure 1 - A calibration equation f
Page 89 and 90: Wire A secondary investigation into
Page 91: [1] Taminger, K. M. B.; and Hafley,
Page 94 and 95: Introduction The analysis of wake v
Page 96 and 97: Figure 2: Screen I mage o f G UI. T
Page 101 and 102: Validation of Novel Rigid Body Fric
Page 103 and 104: forces is implemented in the popula
Page 105 and 106: Figure 2. CAD representation of a t
Page 107 and 108: Results Figure 5. Assembled hydraul
Page 109: References Anitescu, M. (2006). "Op
Page 112 and 113: Multi-stage Joule-Thomson cycles ar
Page 114 and 115: significant change in total compres
Page 116 and 117: The enthalpy (h3) of the 2 nd stage
Page 118 and 119: UA m� ⎛ ε −1 ⎞ ( c nd c st
Page 120 and 121: educed, the temperature range that
Page 122 and 123: 7. Lemmon, E. W.; Huber, M. L.; McL
Page 124 and 125: Throughout each of the run cycles,
Page 126 and 127: and heater adjusted to accommodate
Page 129 and 130: Phaeton Mast Dynamics Mechanical Sy
Page 131 and 132: exposure to the FEMAP with NASTRAN
Page 133 and 134: The irregularity in the plots above
Page 135 and 136: inversion of a particular matrix, t
Page 137: clarified. Additionally, the PMD ki
Page 140 and 141: A. Abstract For hardware to be flig
Page 142 and 143: should be performed at the JWST obs
Page 144 and 145: B. Attenuation and Uncertainty Shoc
Page 146 and 147: 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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A Comparative Study of Type IIb Sup
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Fig. 3.— Cartoon Image of SN blas
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Fig. 4.— Light curve of SN 2008bo
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type IIn Supernova SN 1995N,” 200
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and then can spiral in to the black
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Understanding the Evolution of Supe
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Radio  measurements  of  supe
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In the equations on the p
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SN 2008ax in NGC 4490 SN2008ax is a
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References Chevalier, R. A., “Int
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Computational Fluid Dynamical Model
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context of the k − ɛ model invol
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Figure 3: Experimental results (•
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direction results in the terminal s
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121 (2000). [Blue Ridge Numerics, I
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concentrated our effort specificall
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density, and Ps is a pressure tenso
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Properties of the GEM problem Recon
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Figure 1: Increase in reconnection
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Figure 3: Examples of agreement of
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Reflection and Refraction of Vortex
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Experimental Procedure The left han
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frames in the upper left corner, wh
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Vortex ring reflection. Similarly,
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References L Bernal and J Kwon. Vor
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group started in 1997 with the goal
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I conducted five semi-structured in
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In the example of the guinea pig pr
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explain t his t rend. F rom t alkin
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Research. Washington, DC: Pan Ameri
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Our team has two goals: 1. To put S
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fluctuating humidity, drying winds,
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western border of the Arkansas Rive
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adjusted to less than .4millisecond
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Cacti Experiment 18 has produced 10
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13. What N decomposer's are needed
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Abstract Toxic Offgassing Analysis
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The chambers were sealed and baked
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Tables 4 and 5 show offgassing comp
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there was no dichlorobenzene peak.
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eneficiation reagents. Ionic liquid
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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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