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sider a contingency table with two rows and six columns. a. Find the degrees of freedom. b. Find the critical value for α = 0.025. c. Find the critical value for α = 0.10. Click the icon to view a table of critical values of x². a. The degrees of freedom are an example Get more help . +#1 C I 86°F

sider a contingency table with two rows and six columns. a. Find the degrees of freedom. b. Find the critical value for α = 0.025. c. Find the critical value for α = 0.10. Click the icon to view a table of critical values of x². a. The degrees of freedom are an example Get more help . +#1 C I 86°F

Algebra & Trigonometry with Analytic Geometry
Algebra & Trigonometry with Analytic Geometry
13th Edition
ISBN:9781133382119
Author:Swokowski
Publisher:Swokowski
Chapter4: Polynomial And Rational Functions
Section4.6: Variation
Problem 37E
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Consider a contingency table with two rows and six columns. a. Find the degrees of freedom. b. Find the critical value for α = 0.025. c. Find the critical value for α = 0.10. Click the icon to view a table of critical values of x². a. The degrees of freedom are ew an example Get more help #1 ▲ 86°F C
Transcribed Image Text:Consider a contingency table with two rows and six columns. a. Find the degrees of freedom. b. Find the critical value for α = 0.025. c. Find the critical value for α = 0.10. Click the icon to view a table of critical values of x². a. The degrees of freedom are ew an example Get more help #1 ▲ 86°F C
this Vie ere to search Table of Critical Values of Chi-Square Freedom 1 2 3 4 5 67890 M2BAS RAD 10 11 12 13 14 15 16 17 10 0.995 0.010 0.072 0.207 0.412 0.676 0.989 1.344 1.735 2.156 2.603 3.074 3.565 4.075 4.601 5.142 5.697 6.365 0.99 0.020 0.115 0.297 0.554 #1 ss 3.053 3.571 4.107 0.872 1.239 1.646 2.180 2.088 2.700 2.558 3.247 4.660 5.229 5.812 6.408 7015 0.975 0.95 0.001 0.004 0.051 0.103 0.352 0.216 0.484 0.711 0.831 1.145 O 1.237 1.635 2.167 1.690 2.733 3.325 3.940 3.816 4.404 5.009 5.629 6.262 6.908 7.564 0321 4.575 -5.226 5.892 0.90 0.016 0.211 0.584 1.064 1.610 7.962 8.672 0 200 0.75 0.102 0.575 1.213 1.923 2.675 6.571 8.547 7.261 9.312 10.085 10 865 3.455 2.204 2.833 4.255 3.490 5.071 4.168 11.389 5.899 4.865 6.737 Print 5.578 6.304 13.701 7.584 14.845 8.438 9.299 15.984 18 17.117 10.165 7.790 7.042 11.037 18.245 11.912 12.792 12675 0.25 1.323 2.773 4.108 6.251 5.385 7.779 9236 6.626 19.369 20.489 21605 0.10 2.706 3.841 4.605 5.991 Done O top 10.645 12.592 7.841 9.037 12.017 13362 10.219 14.067 15.507 19.023 16.919 14.684 20.483 18.307 15.987 12.549 0.025 5.024 7.378 7.815 9.348 9.488 11.143 12.833 11.071 0.05 23.542 24.769 25000 14.449 16.013 17.535 23.685 24.996 0.005 6.635 7.879 9.210 10.597 11.345 12.838 13.277 14.860 15.086 16.750 26.296 27.587 30 05 21.920 17275 19.675 23.337 21.026 18.549 24.736 22.362 19.812 21.064 22307 26.119 27.488 0.01 16.812 18.475 20.090 21.666 23.209 24.725 26.217 27.688 29.141 30.578 18.548 20.278 21.955 23.589 25.188 86°F 26.757 28.299 29.819 31.319 32.801 34.267 35.718 27.166 28.845 32.000 33.409 30.191 24 onc 21 536 I
Transcribed Image Text:this Vie ere to search Table of Critical Values of Chi-Square Freedom 1 2 3 4 5 67890 M2BAS RAD 10 11 12 13 14 15 16 17 10 0.995 0.010 0.072 0.207 0.412 0.676 0.989 1.344 1.735 2.156 2.603 3.074 3.565 4.075 4.601 5.142 5.697 6.365 0.99 0.020 0.115 0.297 0.554 #1 ss 3.053 3.571 4.107 0.872 1.239 1.646 2.180 2.088 2.700 2.558 3.247 4.660 5.229 5.812 6.408 7015 0.975 0.95 0.001 0.004 0.051 0.103 0.352 0.216 0.484 0.711 0.831 1.145 O 1.237 1.635 2.167 1.690 2.733 3.325 3.940 3.816 4.404 5.009 5.629 6.262 6.908 7.564 0321 4.575 -5.226 5.892 0.90 0.016 0.211 0.584 1.064 1.610 7.962 8.672 0 200 0.75 0.102 0.575 1.213 1.923 2.675 6.571 8.547 7.261 9.312 10.085 10 865 3.455 2.204 2.833 4.255 3.490 5.071 4.168 11.389 5.899 4.865 6.737 Print 5.578 6.304 13.701 7.584 14.845 8.438 9.299 15.984 18 17.117 10.165 7.790 7.042 11.037 18.245 11.912 12.792 12675 0.25 1.323 2.773 4.108 6.251 5.385 7.779 9236 6.626 19.369 20.489 21605 0.10 2.706 3.841 4.605 5.991 Done O top 10.645 12.592 7.841 9.037 12.017 13362 10.219 14.067 15.507 19.023 16.919 14.684 20.483 18.307 15.987 12.549 0.025 5.024 7.378 7.815 9.348 9.488 11.143 12.833 11.071 0.05 23.542 24.769 25000 14.449 16.013 17.535 23.685 24.996 0.005 6.635 7.879 9.210 10.597 11.345 12.838 13.277 14.860 15.086 16.750 26.296 27.587 30 05 21.920 17275 19.675 23.337 21.026 18.549 24.736 22.362 19.812 21.064 22307 26.119 27.488 0.01 16.812 18.475 20.090 21.666 23.209 24.725 26.217 27.688 29.141 30.578 18.548 20.278 21.955 23.589 25.188 86°F 26.757 28.299 29.819 31.319 32.801 34.267 35.718 27.166 28.845 32.000 33.409 30.191 24 onc 21 536 I
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