Given that,
population mean(u)=1500
sample mean, x =1415.728
standard deviation, s =427.694
number (n)=70
null, Ho: μ=1500
alternate, H1: μ<1500
level of significance, α = 0.02
from standard normal table,left tailed t α/2 =2.093
since our test is left-tailed
reject Ho, if to < -2.093
we use test statistic (t) = x-u/(s.d/sqrt(n))
to =1415.728-1500/(427.694/sqrt(70))
to =-1.649
| to | =1.649
critical value
the value of |t α| with n-1 = 69 d.f is 2.093
we got |to| =1.649 & | t α | =2.093
make decision
hence value of |to | < | t α | and here we do not reject
Ho
p-value :left tail - Ha : ( p < -1.6485 ) = 0.05189
hence value of p0.02 < 0.05189,here we do not reject Ho
ANSWERS
---------------
1.
normal distribution
2.
null, Ho: μ=1500
alternate, H1: μ<1500
test statistic: -1.649
critical value: -2.093
decision: do not reject Ho
p-value: 0.05189
we do not have enough evidence to support the claim that average
number of cycles to failure
is less than 1500.
3.
CONFIDENCE INTERVAL FOR STANDARD DEVIATION
ci = (n-1) s^2 / ᴪ^2 right < σ^2 < (n-1) s^2 / ᴪ^2 left
where,
s = standard deviation
ᴪ^2 right = (1 - confidence level)/2
ᴪ^2 left = 1 - ᴪ^2 right
n = sample size
since alpha =0.01
ᴪ^2 right = (1 - confidence level)/2 = (1 - 0.99)/2 = 0.01/2 =
0.005
ᴪ^2 left = 1 - ᴪ^2 right = 1 - 0.005 = 0.995
the two critical values ᴪ^2 left, ᴪ^2 right at 69 df are 102.9962 ,
42.494
s.d( s )=427.694
sample size(n)=70
confidence interval for σ^2= [ 69 * 182922.1576/102.9962 < σ^2
< 69 * 182922.1576/42.494 ]
= [ 12621628.8769/102.9962 < σ^2 < 12621628.8769/42.4935
]
[ 122544.6072 < σ^2 < 297024.9303 ]
and confidence interval for σ = sqrt(lower) < σ <
sqrt(upper)
= [ sqrt (122544.6072) < σ < sqrt(297024.9303), ]
= [ 350.0637 < σ < 544.9999 ]
The following data represent the number of cycles to failure of aluminum test coupons subjected to...
PLEASE SOLVED THIS PROBLEM BY HAND AND IN
MINITAB:
Construct frequency distribution and histograms using
the failure data
865 1015 885 1594 1000 1416 1501 1115 1310 2130 845 1223 2023 1820 1560 1238 1540 1421 1674 375 1315 1940 990 1055 1502 1109 1016 2265 1269 1120 1764 1468 1258 1481 1102 1910 910 1330 1512 1260 1315 1567 1605 1018 1888 1730 1608 1750 1452 1782 1085 1883 1102 1535 1642 706 798 1203 2215 1890 1522 1578...
Construct a stem-and-leaf display for these data. 2-15. The following data are the numbers of cycles to failure of aluminum test coupons subjected to repeated alternating stress at 21,000 psi, 18 cycles per second: 1115 1310 1567 1883 1223 375 1540 1203 2265 1792 1330 1910 1782 -1522 1055 1764 1502 1258 1315 1085 798 1270 1015 845 1674 1016 1000 10181820 1940 1890 1120 1608 1535 1781 1750 1501 1452 865 2130 1421 1109 1481 2100 1020 110215941730 1238...