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An article in the Journal of Aircraft (1986, Vol. 23, pp.

Applied Statistics and Probability for Engineers | 6th Edition | ISBN: 9781118539712 | Authors: Douglas C. Montgomery, George C. Runger ISBN: 9781118539712 55

Solution for problem 54E Chapter 10.4

Applied Statistics and Probability for Engineers | 6th Edition

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Applied Statistics and Probability for Engineers | 6th Edition | ISBN: 9781118539712 | Authors: Douglas C. Montgomery, George C. Runger

Applied Statistics and Probability for Engineers | 6th Edition

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Problem 54E

Problem 54E

An article in the Journal of Aircraft (1986, Vol. 23, pp. 859–864) described a new equivalent plate analysis method formulation that is capable of modeling aircraft structures such as cranked wing boxes and that produces results similar to the more computationally intensive finite element analysis method. Natural vibration frequencies for the cranked wing box structure are calculated using both methods, and results for the first seven natural frequencies follow:

(a) Do the data suggest that the two methods provide the same mean value for natural vibration frequency? Use α = 0.05. Find the P-value.

(b) Find a 95% confidence interval on the mean difference between the two methods.

Step-by-Step Solution:
Step 1 of 3

Chapter 1: Introducing Stats Statistics- “Set of mathematical procedures for organizing, summarizing, and interpreting data.” Basically, just making sense of numbers for large amounts of data Functions Organize Data  Graphs and Tables Collect and examine information  No calculations or manipulations Visual displays Summarize: Descriptive Stats  Represent information Reduce information to single values  Simplest manipulations and calculations Overall Idea of the data Interpret  Compare summarized in

Step 2 of 3

Chapter 10.4, Problem 54E is Solved
Step 3 of 3

Textbook: Applied Statistics and Probability for Engineers
Edition: 6
Author: Douglas C. Montgomery, George C. Runger
ISBN: 9781118539712

The full step-by-step solution to problem: 54E from chapter: 10.4 was answered by , our top Statistics solution expert on 07/28/17, 07:57AM. This full solution covers the following key subjects: natural, methods, method, results, aircraft. This expansive textbook survival guide covers 97 chapters, and 2005 solutions. This textbook survival guide was created for the textbook: Applied Statistics and Probability for Engineers , edition: 6. Applied Statistics and Probability for Engineers was written by and is associated to the ISBN: 9781118539712. Since the solution to 54E from 10.4 chapter was answered, more than 494 students have viewed the full step-by-step answer. The answer to “An article in the Journal of Aircraft (1986, Vol. 23, pp. 859–864) described a new equivalent plate analysis method formulation that is capable of modeling aircraft structures such as cranked wing boxes and that produces results similar to the more computationally intensive finite element analysis method. Natural vibration frequencies for the cranked wing box structure are calculated using both methods, and results for the first seven natural frequencies follow: (a) Do the data suggest that the two methods provide the same mean value for natural vibration frequency? Use ? = 0.05. Find the P-value.(b) Find a 95% confidence interval on the mean difference between the two methods.” is broken down into a number of easy to follow steps, and 107 words.

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An article in the Journal of Aircraft (1986, Vol. 23, pp.