Specifications for an aircraft bolt require that the ultimate tensile strength be at least 18 kN. It is known that 10% of the bolts have strengths less than 18.3 kN and that 5% of the bolts have strengths greater than 19.76 kN. It is also known that the strengths of these bolts are normally distributed. a. Find the mean of the strengths. [Select] b. Find the standard deviation of the strengths. [Select] b. About what proportion of the bolts meet the strength specification? [Select]

MATLAB: An Introduction with Applications
6th Edition
ISBN:9781119256830
Author:Amos Gilat
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Specifications for an aircraft bolt require that the ultimate tensile
strength be at least 18 kN. It is known that 10% of the bolts have
strengths less than 18.3 kN and that 5% of the bolts have strengths
greater than 19.76 kN. It is also known that the strengths of
these bolts are normally distributed.
a. Find the mean of the strengths. [Select]
b. Find the standard deviation of the strengths.
[Select]
b. About what proportion of the bolts meet the strength specification?
[Select]
Transcribed Image Text:Specifications for an aircraft bolt require that the ultimate tensile strength be at least 18 kN. It is known that 10% of the bolts have strengths less than 18.3 kN and that 5% of the bolts have strengths greater than 19.76 kN. It is also known that the strengths of these bolts are normally distributed. a. Find the mean of the strengths. [Select] b. Find the standard deviation of the strengths. [Select] b. About what proportion of the bolts meet the strength specification? [Select]
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