Difference between revisions of "Phi angle in CM frame for different runs"
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1.4 < Q^2 < 1.8 1.13< W <1.17 | 1.4 < Q^2 < 1.8 1.13< W <1.17 | ||
Revision as of 01:20, 8 July 2008
EC_total, vs , missing mass, vs
- Electron Momentum vs EC_total
- Missing Mass
- vs
Phi lab
The angle is (0, 360).
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Phi CM
The phi angle after rotation and transformation to the CM frame
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Correlation plots with , and
The angle is (0, 360).
| vs | vs | vs |
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Same table as above but with the cut 1.0 < W < 1.5
| vs | vs | vs |
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Same table as above but with the cuts 1.0 < W < 1.25 GeV , 20 MeV bins in W and 15 degree bins in
| vs | vs | vs |
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Same table as above but with the cuts 1.0 < W < 1.5 GeV and -0.2 < < 0
| vs | vs | vs |
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Insert the same table as above but with the cuts 1.15 < W < 1.25 GeV and -0.1 < < 0, 20 MeV bins in W and 15 degree bins in
| vs | vs | vs |
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Insert the same table as above but with the cuts W < 1.25 GeV and -0.1 < < 0, 20 MeV bins in W and 15 degree bins in
| vs | vs | vs |
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Phi_angle_in_CM_Frame for different cuts
Used 1735 files. The following cuts are applied: , and EC cuts.
Insert plot of M_x and W to show cuts
Then insert phi -vs- theta
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1.4 < Q^2 < 1.8 1.13< W <1.17
cos(theta_pi) phi(pi+) dsigma/dOmega Data errors Systematic errors
dimensionless degree mcbn/sterad mcbn/sterad mcbn/sterad
0.3 7.5 0.23121 0.03482 0.0881
0.3 22.5 0.26869 0.06138 0.10488
0.3 127.5 0.8338 0.0946 0.00803
0.3 142.5 0.75189 0.07331 0.01173
0.3 157.5 0.51962 0.06065 0.01193
0.3 172.5 0.51907 0.05707 0.00719
0.3 187.5 0.52325 0.0595 0.01046
0.3 202.5 0.62424 0.06558 0.03508
0.3 217.5 0.7166 0.07414 0.01469
0.3 232.5 0.88201 0.08297 0.00386
0.3 247.5 0.93528 0.10613 0.02175
0.3 337.5 0.25797 0.05635 0.13169
0.3 352.5 0.14197 0.02875 0.0614
0.5 7.5 0.179 0.02725 0.00658
0.5 22.5 0.30852 0.04432 0.03407
0.5 37.5 0.5206 0.07215 0.01749
0.5 97.5 1.12986 0.08825 0.01938
0.5 112.5 1.09252 0.10256 0.06597
0.5 127.5 0.9763 0.08506 0.01533
0.5 142.5 0.79077 0.07363 0.00473
0.5 157.5 0.59172 0.06821 0.00877
0.5 172.5 0.58077 0.06074 0.00335
0.5 187.5 0.50715 0.06304 0.00339
0.5 202.5 0.70732 0.07237 0.00357
0.5 217.5 0.88784 0.06989 0.00937
0.5 232.5 0.94631 0.08343 0.01849
0.5 247.5 1.00856 0.10138 0.0134
0.5 262.5 1.10049 0.10723 0.02199
0.5 292.5 1.03853 0.12326 0.02233
0.5 307.5 0.79737 0.09255 0.02999
0.5 322.5 0.47804 0.05456 0.06938
0.5 337.5 0.22268 0.0358 0.01679
0.5 352.5 0.1918 0.02612 0.00524
0.7 7.5 0.30337 0.0306 0.00398
0.7 22.5 0.30258 0.03349 0.00667
0.7 37.5 0.46911 0.04764 0.01997
0.7 52.5 0.57902 0.063 0.00552
0.7 67.5 0.97887 0.08763 0.00523
0.7 82.5 1.03443 0.08417 0.03062
0.7 97.5 1.17882 0.09053 0.00646
0.7 112.5 0.77904 0.07607 0.00368
0.7 127.5 0.82434 0.07262 0.00653
0.7 142.5 0.59427 0.06226 0.03665
0.7 157.5 0.74611 0.06865 0.02487
0.7 172.5 0.66586 0.07026 0.0199
0.7 187.5 0.69131 0.066 0.02584
0.7 202.5 0.68681 0.06741 0.04256
0.7 217.5 0.86021 0.07673 0.00771
0.7 232.5 0.71823 0.06485 0.00523
0.7 247.5 1.01875 0.07804 0.01166
0.7 262.5 0.96511 0.08223 0.01259
0.7 277.5 0.88611 0.07973 0.00523
0.7 292.5 0.78151 0.0745 0.02159
0.7 307.5 0.567 0.05758 0.0221
0.7 322.5 0.54127 0.0554 0.01185
0.7 337.5 0.29805 0.03881 0.00821
0.7 352.5 0.31606 0.03496 0.02255
0.9 7.5 0.46812 0.04844 0.00794
0.9 22.5 0.43017 0.04467 0.0078
0.9 37.5 0.52086 0.05095 0.00808
0.9 52.5 0.46469 0.04821 0.00821
0.9 67.5 0.72754 0.06163 0.00574
0.9 82.5 0.74611 0.0728 0.00751
0.9 97.5 0.83247 0.06562 0.01103
0.9 112.5 0.66814 0.06182 0.00379
0.9 127.5 0.86453 0.06943 0.00463
0.9 142.5 0.62351 0.06141 0.00539
0.9 157.5 0.67536 0.06566 0.01181
0.9 172.5 0.7917 0.07021 0.00883
0.9 187.5 0.67283 0.06538 0.00671
0.9 202.5 0.69394 0.06482 0.01046
0.9 217.5 0.93148 0.07572 0.01137
0.9 232.5 0.85828 0.07093 0.011
0.9 247.5 0.92765 0.07794 0.00996
0.9 262.5 0.82349 0.07194 0.00628
0.9 277.5 0.78016 0.06459 0.01851
0.9 292.5 0.70836 0.06817 0.01541
0.9 307.5 0.60915 0.05905 0.01231
0.9 322.5 0.49794 0.04657 0.00566
0.9 337.5 0.4766 0.05517 0.00839
0.9 352.5 0.74038 0.0689 0.01111