Chapter 9 : Relationship of WingSize size to selected variables
Raw data Listing

Obs continent latitude females seF males seM ratio seR
1 na 35.5 901 2.5 797 3.8 0.831 0.010
2 na 37.0 896 3.5 806 3.0 0.834 0.014
3 na 38.6 906 3.0 812 3.2 0.836 0.012
4 na 40.7 907 3.5 807 3.2 0.833 0.013
5 na 40.9 898 3.6 818 2.7 0.830 0.012
6 na 42.4 893 3.4 809 3.3 0.828 0.015
7 na 45.0 913 4.3 810 4.3 0.834 0.024
8 na 46.8 915 3.8 819 3.3 0.825 0.014
9 na 48.8 927 2.0 800 4.9 0.832 0.009
10 na 49.8 924 4.5 823 2.2 0.824 0.011
11 na 50.8 930 3.4 814 4.1 0.826 0.013
12 eu 36.4 905 6.1 789 5.9 0.822 0.016
13 eu 39.3 889 4.7 803 3.5 0.809 0.021
14 eu 41.3 915 2.1 812 3.7 0.821 0.007
15 eu 43.4 930 2.6 820 3.1 0.831 0.016
16 eu 45.5 895 4.4 808 2.9 0.821 0.017
17 eu 47.3 926 3.2 815 6.2 0.826 0.010
18 eu 48.5 944 4.8 855 3.1 0.825 0.032
19 eu 50.4 925 3.2 842 4.3 0.820 0.013
20 eu 52.1 920 3.9 819 3.1 0.834 0.019
21 eu 56.1 934 4.2 839 4.4 0.825 0.012


Chapter 9 : Relationship of WingSize size to selected variables
Processed data Listing

Obs continent latitude sex Wingsize se ID group1 group2 group3 group4 X1 X2 X3 X4
1 eu 39.3 Female 889 4.7 F 1 0 0 0 39.3 0.0 0.0 0.0
2 eu 45.5 Female 895 4.4 F 1 0 0 0 45.5 0.0 0.0 0.0
3 eu 36.4 Female 905 6.1 F 1 0 0 0 36.4 0.0 0.0 0.0
4 eu 41.3 Female 915 2.1 F 1 0 0 0 41.3 0.0 0.0 0.0
5 eu 52.1 Female 920 3.9 F 1 0 0 0 52.1 0.0 0.0 0.0
6 eu 50.4 Female 925 3.2 F 1 0 0 0 50.4 0.0 0.0 0.0
7 eu 47.3 Female 926 3.2 F 1 0 0 0 47.3 0.0 0.0 0.0
8 eu 43.4 Female 930 2.6 F 1 0 0 0 43.4 0.0 0.0 0.0
9 eu 56.1 Female 934 4.2 F 1 0 0 0 56.1 0.0 0.0 0.0
10 eu 48.5 Female 944 4.8 F 1 0 0 0 48.5 0.0 0.0 0.0
11 eu 36.4 Male 789 5.9 M 0 1 0 0 0.0 36.4 0.0 0.0
12 eu 39.3 Male 803 3.5 M 0 1 0 0 0.0 39.3 0.0 0.0
13 eu 45.5 Male 808 2.9 M 0 1 0 0 0.0 45.5 0.0 0.0
14 eu 41.3 Male 812 3.7 M 0 1 0 0 0.0 41.3 0.0 0.0
15 eu 47.3 Male 815 6.2 M 0 1 0 0 0.0 47.3 0.0 0.0
16 eu 52.1 Male 819 3.1 M 0 1 0 0 0.0 52.1 0.0 0.0
17 eu 43.4 Male 820 3.1 M 0 1 0 0 0.0 43.4 0.0 0.0
18 eu 56.1 Male 839 4.4 M 0 1 0 0 0.0 56.1 0.0 0.0
19 eu 50.4 Male 842 4.3 M 0 1 0 0 0.0 50.4 0.0 0.0
20 eu 48.5 Male 855 3.1 M 0 1 0 0 0.0 48.5 0.0 0.0
21 na 42.4 Female 893 3.4 f 0 0 1 0 0.0 0.0 42.4 0.0
22 na 37.0 Female 896 3.5 f 0 0 1 0 0.0 0.0 37.0 0.0
23 na 40.9 Female 898 3.6 f 0 0 1 0 0.0 0.0 40.9 0.0
24 na 35.5 Female 901 2.5 f 0 0 1 0 0.0 0.0 35.5 0.0
25 na 38.6 Female 906 3.0 f 0 0 1 0 0.0 0.0 38.6 0.0
26 na 40.7 Female 907 3.5 f 0 0 1 0 0.0 0.0 40.7 0.0
27 na 45.0 Female 913 4.3 f 0 0 1 0 0.0 0.0 45.0 0.0
28 na 46.8 Female 915 3.8 f 0 0 1 0 0.0 0.0 46.8 0.0
29 na 49.8 Female 924 4.5 f 0 0 1 0 0.0 0.0 49.8 0.0
30 na 48.8 Female 927 2.0 f 0 0 1 0 0.0 0.0 48.8 0.0
31 na 50.8 Female 930 3.4 f 0 0 1 0 0.0 0.0 50.8 0.0
32 na 35.5 Male 797 3.8 m 0 0 0 1 0.0 0.0 0.0 35.5
33 na 48.8 Male 800 4.9 m 0 0 0 1 0.0 0.0 0.0 48.8
34 na 37.0 Male 806 3.0 m 0 0 0 1 0.0 0.0 0.0 37.0
35 na 40.7 Male 807 3.2 m 0 0 0 1 0.0 0.0 0.0 40.7
36 na 42.4 Male 809 3.3 m 0 0 0 1 0.0 0.0 0.0 42.4
37 na 45.0 Male 810 4.3 m 0 0 0 1 0.0 0.0 0.0 45.0
38 na 38.6 Male 812 3.2 m 0 0 0 1 0.0 0.0 0.0 38.6
39 na 50.8 Male 814 4.1 m 0 0 0 1 0.0 0.0 0.0 50.8
40 na 40.9 Male 818 2.7 m 0 0 0 1 0.0 0.0 0.0 40.9
41 na 46.8 Male 819 3.3 m 0 0 0 1 0.0 0.0 0.0 46.8
42 na 49.8 Male 823 2.2 m 0 0 0 1 0.0 0.0 0.0 49.8


Chapter 9 : Relationship of WingSize size to selected variables
Plot of the raw data with ID variable

                                         Plot of Wingsize*latitude.  Symbol is value of ID.                                         
                                                                                                                                    
Wingsize |                                                                                                                          
         |                                                                                                                          
     960 +                                                                                                                          
         |                                                                                                                          
         |                                                                                                                          
         |                                                                                                                          
         |                                                                         F                                                
     940 +                                                                                                                          
         |                                                                                                               F          
         |                                               F                                    f                                     
         |                                                                   F      f                                               
         |                                                                               f  F                                       
     920 +                                                                                           F                              
         |                                     F                          f                                                         
         |                                                       f                                                                  
         |                       f          f                                                                                       
         |            F                                                                                                             
     900 +        f                          f                                                                                      
         |               f                                          F                                                               
         |                                          f                                                                               
         |                           F                                                                                              
         |                                                                                                                          
     880 +                                                                                                                          
         |                                                                                                                          
         |                                                                                                                          
         |                                                                                                                          
         |                                                                                                                          
     860 +                                                                                                                          
         |                                                                         M                                                
         |                                                                                                                          
         |                                                                                                                          
         |                                                                                  M                                       
     840 +                                                                                                               M          
         |                                                                                                                          
         |                                                                                                                          
         |                                                                                                                          
         |                                                                               m                                          
     820 +                                   m           M                m                          M                              
         |                                                                   M                m                                     
         |                       m             M                 m                                                                  
         |               m                  m       m               M                                                               
         |                           M                                                                                              
     800 +                                                                          m                                               
         |        m                                                                                                                 
         |                                                                                                                          
         |            M                                                                                                             
         |                                                                                                                          
     780 +                                                                                                                          
         |                                                                                                                          
         -+---------+---------+---------+---------+---------+---------+---------+---------+---------+---------+---------+---------+-
         34        36        38        40        42        44        46        48        50        52        54        56        58 
                                                                                                                                    
                                                                   latitude                                                         


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on Latitude one line

The REG Procedure
Model: MODEL1
Dependent Variable: Wingsize

Number of Observations Read 42
Number of Observations Used 42

Analysis of Variance
Source DF Sum of
Squares
Mean
Square
F Value Pr > F
Model 1 4621.44765 4621.44765 1.72 0.1971
Error 40 107425 2685.62571    
Corrected Total 41 112046      

Root MSE 51.82302 R-Square 0.0412
Dependent Mean 864.52381 Adj R-Sq 0.0173
Coeff Var 5.99440    

Parameter Estimates
Variable DF Parameter
Estimate
Standard
Error
t Value Pr > |t|
Intercept 1 780.53173 64.52572 12.10 <.0001
latitude 1 1.88323 1.43561 1.31 0.1971


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on Latitude separate intercepts

The REG Procedure
Model: MODEL1
Dependent Variable: Wingsize

Number of Observations Read 42
Number of Observations Used 42

Analysis of Variance
Source DF Sum of
Squares
Mean
Square
F Value Pr > F
Model 4 107409 26852 214.22 <.0001
Error 37 4637.94684 125.34991    
Corrected Total 41 112046      

Root MSE 11.19598 R-Square 0.9586
Dependent Mean 864.52381 Adj R-Sq 0.9541
Coeff Var 1.29505    


Model is not full rank. Least-squares solutions for the parameters are not unique. Some statistics will be misleading. A reported DF of 0 or B means that the estimate is biased.


The following parameters have been set to 0, since the variables are a linear combination of other variables as shown.

group4 = Intercept - group1 - group2 - group3

Parameter Estimates
Variable DF Parameter
Estimate
Standard
Error
t Value Pr > |t|
Intercept B 732.83456 14.25644 51.40 <.0001
latitude 1 1.79261 0.31988 5.60 <.0001
group1 B 102.95163 4.96921 20.72 <.0001
group2 B 4.85163 4.96921 0.98 0.3352
group3 B 99.54545 4.77398 20.85 <.0001
group4 0 0 . . .


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on Latitude separate slopes and intercepts

The REG Procedure
Model: MODEL1
Dependent Variable: Wingsize

Number of Observations Read 42
Number of Observations Used 42

Analysis of Variance
Source DF Sum of
Squares
Mean
Square
F Value Pr > F
Model 7 107913 15416 126.80 <.0001
Error 34 4133.68477 121.57896    
Corrected Total 41 112046      

Root MSE 11.02629 R-Square 0.9631
Dependent Mean 864.52381 Adj R-Sq 0.9555
Coeff Var 1.27542    


Model is not full rank. Least-squares solutions for the parameters are not unique. Some statistics will be misleading. A reported DF of 0 or B means that the estimate is biased.


The following parameters have been set to 0, since the variables are a linear combination of other variables as shown.

group4 = Intercept - group1 - group2 - group3
X4 = latitude - X1 - X2 - X3

Parameter Estimates
Variable DF Parameter
Estimate
Standard
Error
t Value Pr > |t|
Intercept B 779.86417 28.73352 27.14 <.0001
latitude B 0.70648 0.65913 1.07 0.2913
group1 B 56.32623 40.15128 1.40 0.1697
group2 B -72.93864 40.15128 -1.82 0.0781
group3 B 39.43235 40.63533 0.97 0.3387
group4 0 0 . . .
X1 B 1.07735 0.89439 1.20 0.2367
X2 B 1.75441 0.89439 1.96 0.0580
X3 B 1.38829 0.93216 1.49 0.1456
X4 0 0 . . .


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on indicator variables with GLM

The GLM Procedure

Class Level Information
Class Levels Values
ID 4 F M f m

Number of Observations Read 42
Number of Observations Used 42


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on indicator variables with GLM

The GLM Procedure
 
Dependent Variable: Wingsize

Source DF Sum of Squares Mean Square F Value Pr > F
Model 7 107912.7914 15416.1131 126.80 <.0001
Error 34 4133.6848 121.5790    
Corrected Total 41 112046.4762      

R-Square Coeff Var Root MSE Wingsize Mean
0.963107 1.275417 11.02629 864.5238

Source DF Type I SS Mean Square F Value Pr > F
latitude 1 4621.4476 4621.4476 38.01 <.0001
ID 3 102787.0817 34262.3606 281.81 <.0001
latitude*ID 3 504.2621 168.0874 1.38 0.2647

Source DF Type III SS Mean Square F Value Pr > F
latitude 1 3772.720501 3772.720501 31.03 <.0001
ID 3 1524.400042 508.133347 4.18 0.0127
latitude*ID 3 504.262074 168.087358 1.38 0.2647

Parameter Estimate   Standard Error t Value Pr > |t|
Intercept 779.8641724 B 28.73352016 27.14 <.0001
latitude 0.7064751 B 0.65913492 1.07 0.2913
ID F 56.3262256 B 40.15127904 1.40 0.1697
ID M -72.9386446 B 40.15127904 -1.82 0.0781
ID f 39.4323542 B 40.63533390 0.97 0.3387
ID m 0.0000000 B . . .
latitude*ID F 1.0773529 B 0.89438968 1.20 0.2367
latitude*ID M 1.7544085 B 0.89438968 1.96 0.0580
latitude*ID f 1.3882933 B 0.93215755 1.49 0.1456
latitude*ID m 0.0000000 B . . .


The X'X matrix has been found to be singular, and a generalized inverse was used to solve the normal equations. Terms whose estimates are followed by the letter 'B' are not uniquely estimable.


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on original variables with GLM

The GLM Procedure

Class Level Information
Class Levels Values
sex 2 Female Male
continent 2 eu na

Number of Observations Read 42
Number of Observations Used 42


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on original variables with GLM

The GLM Procedure
 
Dependent Variable: Wingsize

Source DF Sum of Squares Mean Square F Value Pr > F
Model 7 107912.7914 15416.1131 126.80 <.0001
Error 34 4133.6848 121.5790    
Corrected Total 41 112046.4762      

R-Square Coeff Var Root MSE Wingsize Mean
0.963107 1.275417 11.02629 864.5238

Source DF Type I SS Mean Square F Value Pr > F
latitude 1 4621.4476 4621.4476 38.01 <.0001
sex 1 102613.7143 102613.7143 844.01 <.0001
continent 1 167.8953 167.8953 1.38 0.2481
sex*continent 1 5.4721 5.4721 0.05 0.8333
latitude*sex 1 21.7609 21.7609 0.18 0.6749
latitude*continent 1 158.3395 158.3395 1.30 0.2618
latitud*sex*continen 1 324.1617 324.1617 2.67 0.1117

Source DF Type III SS Mean Square F Value Pr > F
latitude 1 3772.720501 3772.720501 31.03 <.0001
sex 1 1073.113225 1073.113225 8.83 0.0054
continent 1 118.440410 118.440410 0.97 0.3306
sex*continent 1 304.296390 304.296390 2.50 0.1229
latitude*sex 1 38.441861 38.441861 0.32 0.5776
latitude*continent 1 158.339480 158.339480 1.30 0.2618
latitud*sex*continen 1 324.161738 324.161738 2.67 0.1117

Parameter Estimate   Standard Error t Value Pr > |t|
Intercept 779.8641724 B 28.73352016 27.14 <.0001
latitude 0.7064751 B 0.65913492 1.07 0.2913
sex Female 39.4323542 B 40.63533390 0.97 0.3387
sex Male 0.0000000 B . . .
continent eu -72.9386446 B 40.15127904 -1.82 0.0781
continent na 0.0000000 B . . .
sex*continent Female eu 89.8325160 B 56.78248337 1.58 0.1229
sex*continent Female na 0.0000000 B . . .
sex*continent Male eu 0.0000000 B . . .
sex*continent Male na 0.0000000 B . . .
latitude*sex Female 1.3882933 B 0.93215755 1.49 0.1456
latitude*sex Male 0.0000000 B . . .
latitude*continent eu 1.7544085 B 0.89438968 1.96 0.0580
latitude*continent na 0.0000000 B . . .
latitud*sex*continen Female eu -2.0653489 B 1.26485802 -1.63 0.1117
latitud*sex*continen Female na 0.0000000 B . . .
latitud*sex*continen Male eu 0.0000000 B . . .
latitud*sex*continen Male na 0.0000000 B . . .


The X'X matrix has been found to be singular, and a generalized inverse was used to solve the normal equations. Terms whose estimates are followed by the letter 'B' are not uniquely estimable.


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on original variables with GLM model reordered

The GLM Procedure

Class Level Information
Class Levels Values
sex 2 Female Male
continent 2 eu na

Number of Observations Read 42
Number of Observations Used 42


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on original variables with GLM model reordered

The GLM Procedure
 
Dependent Variable: Wingsize

Source DF Sum of Squares Mean Square F Value Pr > F
Model 7 107912.7914 15416.1131 126.80 <.0001
Error 34 4133.6848 121.5790    
Corrected Total 41 112046.4762      

R-Square Coeff Var Root MSE Wingsize Mean
0.963107 1.275417 11.02629 864.5238

Source DF Type I SS Mean Square F Value Pr > F
latitude 1 4621.4476 4621.4476 38.01 <.0001
sex 1 102613.7143 102613.7143 844.01 <.0001
latitude*sex 1 15.6052 15.6052 0.13 0.7224
continent 1 167.8953 167.8953 1.38 0.2481
latitude*continent 1 158.3395 158.3395 1.30 0.2618
sex*continent 1 11.6278 11.6278 0.10 0.7590
latitud*sex*continen 1 324.1617 324.1617 2.67 0.1117

Source DF Type III SS Mean Square F Value Pr > F
latitude 1 3772.720501 3772.720501 31.03 <.0001
sex 1 1073.113225 1073.113225 8.83 0.0054
latitude*sex 1 38.441861 38.441861 0.32 0.5776
continent 1 118.440410 118.440410 0.97 0.3306
latitude*continent 1 158.339480 158.339480 1.30 0.2618
sex*continent 1 304.296390 304.296390 2.50 0.1229
latitud*sex*continen 1 324.161738 324.161738 2.67 0.1117

Parameter Estimate   Standard Error t Value Pr > |t|
Intercept 779.8641724 B 28.73352016 27.14 <.0001
latitude 0.7064751 B 0.65913492 1.07 0.2913
sex Female 39.4323542 B 40.63533390 0.97 0.3387
sex Male 0.0000000 B . . .
latitude*sex Female 1.3882933 B 0.93215755 1.49 0.1456
latitude*sex Male 0.0000000 B . . .
continent eu -72.9386446 B 40.15127904 -1.82 0.0781
continent na 0.0000000 B . . .
latitude*continent eu 1.7544085 B 0.89438968 1.96 0.0580
latitude*continent na 0.0000000 B . . .
sex*continent Female eu 89.8325160 B 56.78248337 1.58 0.1229
sex*continent Female na 0.0000000 B . . .
sex*continent Male eu 0.0000000 B . . .
sex*continent Male na 0.0000000 B . . .
latitud*sex*continen Female eu -2.0653489 B 1.26485802 -1.63 0.1117
latitud*sex*continen Female na 0.0000000 B . . .
latitud*sex*continen Male eu 0.0000000 B . . .
latitud*sex*continen Male na 0.0000000 B . . .


The X'X matrix has been found to be singular, and a generalized inverse was used to solve the normal equations. Terms whose estimates are followed by the letter 'B' are not uniquely estimable.


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize - best model?

The GLM Procedure

Class Level Information
Class Levels Values
sex 2 Female Male
continent 2 eu na

Number of Observations Read 42
Number of Observations Used 42


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize - best model?

The GLM Procedure
 
Dependent Variable: Wingsize

Source DF Sum of Squares Mean Square F Value Pr > F
Model 2 107235.1619 53617.5810 434.62 <.0001
Error 39 4811.3143 123.3670    
Corrected Total 41 112046.4762      

R-Square Coeff Var Root MSE Wingsize Mean
0.957060 1.284762 11.10707 864.5238

Source DF Type I SS Mean Square F Value Pr > F
latitude 1 4621.4476 4621.4476 37.46 <.0001
sex 1 102613.7143 102613.7143 831.78 <.0001

Source DF Type III SS Mean Square F Value Pr > F
latitude 1 4621.4476 4621.4476 37.46 <.0001
sex 1 102613.7143 102613.7143 831.78 <.0001

Parameter Estimate   Standard Error t Value Pr > |t|
Intercept 731.1031578 B 13.93539338 52.46 <.0001
latitude 1.8832305   0.30769045 6.12 <.0001
sex Female 98.8571429 B 3.42771661 28.84 <.0001
sex Male 0.0000000 B . . .


The X'X matrix has been found to be singular, and a generalized inverse was used to solve the normal equations. Terms whose estimates are followed by the letter 'B' are not uniquely estimable.


Chapter 9 : Relationship of WingSize size to selected variables
Residual plot with sex ID variable

                                          Plot of resid*latitude.  Symbol is value of sex.                                          
                                                                                                                                    
resid |                                                                                                                             
      |                                                                                                                             
   40 +                                                                                                                             
      |                                                                                                                             
      |                                                                                                                             
      |                                                                                                                             
      |                                                                                                                             
      |                                                                           M                                                 
      |                                                                                                                             
   30 +                                                                                                                             
      |                                                                                                                             
      |                                                                                                                             
      |                                                                                                                             
      |                                                                                                                             
      |                                                                           F                                                 
      |                                                                                                                             
   20 +                                                                                                                             
      |                                                 F                                                                           
      |                                                                                                                             
      |                                                                                    M                                        
      |                                                                                                                             
      |                                                                                                                             
      |                                                                                                                             
   10 +                                     M                                                                                       
      |                         M                                                                                                   
      |              F                        F         M                   F                                                       
      |                 M                                                          F                                                
      |          F                                                                           F                                      
      |                         F             M                                                                         M           
      |                                                                                                                             
    0 +                                    F                             M              F  F                                        
      |          M                  M      M       M            F                       M                               F           
      |                                                                  F                                                          
      |                 F                                                                                                           
      |                                                         M           M                                                       
      |                                                                                                                             
      |                                     F                      M                                F                               
  -10 +              M                                                                              M                               
      |                                                                                                                             
      |                                                                                      M                                      
      |                             F                                                                                               
      |                                                                                                                             
      |                                            F                                                                                
      |                                                                                                                             
  -20 +                                                            F                                                                
      |                                                                                                                             
      |                                                                            M                                                
      |                                                                                                                             
      |                                                                                                                             
      |                                                                                                                             
      |                                                                                                                             
  -30 +                                                                                                                             
      |                                                                                                                             
      ---+---------+---------+---------+---------+---------+---------+---------+---------+---------+---------+---------+---------+--
        34        36        38        40        42        44        46        48        50        52        54        56        58  
                                                                                                                                    
                                                                 latitude                                                           


Chapter 9 : Relationship of WingSize size to selected variables
Residual plot with sex ID variable

The UNIVARIATE Procedure
Variable: resid

Moments
N 42 Sum Weights 42
Mean 0 Sum Observations 0
Std Deviation 10.8327803 Variance 117.349128
Skewness 0.48361594 Kurtosis 1.3897594
Uncorrected SS 4811.31426 Corrected SS 4811.31426
Coeff Variation . Std Error Mean 1.67153428

Basic Statistical Measures
Location Variability
Mean 0.00000 Std Deviation 10.83278
Median -0.49449 Variance 117.34913
Mode . Range 55.56497
    Interquartile Range 11.06584

Tests for Location: Mu0=0
Test Statistic p Value
Student's t t 0 Pr > |t| 1.0000
Sign M -1 Pr >= |M| 0.8776
Signed Rank S -14.5 Pr >= |S| 0.8587

Tests for Normality
Test Statistic p Value
Shapiro-Wilk W 0.966654 Pr < W 0.2539
Kolmogorov-Smirnov D 0.108445 Pr > D >0.1500
Cramer-von Mises W-Sq 0.084476 Pr > W-Sq 0.1825
Anderson-Darling A-Sq 0.505494 Pr > A-Sq 0.2004

Quantiles (Definition 5)
Quantile Estimate
100% Max 32.560163
99% 32.560163
95% 18.307496
90% 9.872715
75% Q3 5.217314
50% Median -0.494492
25% Q1 -5.848530
10% -12.771267
5% -16.809274
1% -23.004806
0% Min -23.004806

Extreme Observations
Lowest Highest
Value Obs Value Obs
-23.0048 33 9.87271 40
-20.6473 2 15.98203 19
-16.8093 21 18.30750 8
-14.9713 1 22.70302 10
-12.7713 39 32.56016 20

   Stem Leaf                     #  Boxplot                        Normal Probability Plot                                          
      3 3                        1     0        32.5+                                               *                               
      2                                             |                                                 ++                            
      2 3                        1     0            |                                           *+++++                              
      1 68                       2     |            |                                       **+++                                   
      1 0                        1     |            |                                   ++++                                        
      0 5567778                  7  +-----+         |                              +*******                                         
      0 00023344                 8  |  +  |         |                         +*****                                                
     -0 4322222110              10  *-----*         |                    ******                                                     
     -0 99865                    5  +-----+         |                ****+                                                          
     -1 310                      3     |            |           *+***                                                               
     -1 75                       2     |            |       +++*+                                                                   
     -2 31                       2     0       -22.5+  +*+++*                                                                       
        ----+----+----+----+                         +----+----+----+----+----+----+----+----+----+----+                            
    Multiply Stem.Leaf by 10**+1                         -2        -1         0        +1        +2                                 
                                                                                                                                    
                                                                                                                                    


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on Latitude separate slopes and intercepts

The REG Procedure
Model: MODEL1
Dependent Variable: Wingsize

Number of Observations Read 42
Number of Observations Used 42


No intercept in model. R-Square is redefined.

Analysis of Variance
Source DF Sum of
Squares
Mean
Square
F Value Pr > F
Model 8 31498772 3937347 32385.1 <.0001
Error 34 4133.68477 121.57896    
Uncorrected Total 42 31502906      

Root MSE 11.02629 R-Square 0.9999
Dependent Mean 864.52381 Adj R-Sq 0.9998
Coeff Var 1.27542    

Parameter Estimates
Variable DF Parameter
Estimate
Standard
Error
t Value Pr > |t|
group1 1 836.19040 28.04479 29.82 <.0001
group2 1 706.92553 28.04479 25.21 <.0001
group3 1 819.29653 28.73352 28.51 <.0001
group4 1 779.86417 28.73352 27.14 <.0001
X1 1 1.78383 0.60454 2.95 0.0057
X2 1 2.46088 0.60454 4.07 0.0003
X3 1 2.09477 0.65913 3.18 0.0032
X4 1 0.70648 0.65913 1.07 0.2913


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on original variables with GLM

The GLM Procedure

Class Level Information
Class Levels Values
sex 2 Female Male
continent 2 eu na

Number of Observations Read 42
Number of Observations Used 42


Chapter 9 : Relationship of WingSize size to selected variables
Fit of WingSize on original variables with GLM

The GLM Procedure
 
Dependent Variable: Wingsize

Source DF Sum of Squares Mean Square F Value Pr > F
Model 8 31498772.32 3937346.54 32385.1 <.0001
Error 34 4133.68 121.58    
Uncorrected Total 42 31502906.00      

R-Square Coeff Var Root MSE Wingsize Mean
0.963107 1.275417 11.02629 864.5238

Source DF Type I SS Mean Square F Value Pr > F
sex*continent 4 31494331.57 7873582.89 64761.1 <.0001
latitud*sex*continen 4 4440.74 1110.19 9.13 <.0001

Source DF Type III SS Mean Square F Value Pr > F
sex*continent 4 373743.1513 93435.7878 768.52 <.0001
latitud*sex*continen 4 4440.7425 1110.1856 9.13 <.0001

Parameter Estimate Standard Error t Value Pr > |t|
sex*continent Female eu 836.1903980 28.04478612 29.82 <.0001
sex*continent Female na 819.2965266 28.73352016 28.51 <.0001
sex*continent Male eu 706.9255278 28.04478612 25.21 <.0001
sex*continent Male na 779.8641724 28.73352016 27.14 <.0001
latitud*sex*continen Female eu 1.7838280 0.60454450 2.95 0.0057
latitud*sex*continen Female na 2.0947684 0.65913492 3.18 0.0032
latitud*sex*continen Male eu 2.4608836 0.60454450 4.07 0.0003
latitud*sex*continen Male na 0.7064751 0.65913492 1.07 0.2913