Acommercial passenger aircraft manufacturer would like to make aircraft fuselages with fibre-reinforced polymer composite materials. the required production rate is 10 units per month. the fuselage sections are 8m in diameter and 20m long. the composite fuselage structure must be manufactured with high quality and consistency to pass the stringent certification process. (a) what material system (matrix and reinforcement) would you select and for what reasons? (b) which material forms (e. g. fibre preform, prepreg etc.) and corresponding manufacturing process would you recommend? state the specific reasons for each recommendation.

answer:

it thinks that you spelled something wrong.

explanation:

answer:

is a

explanation:

answer:

the formula for amps is watts divided by volts. to use the chart, cover up the a with your finger and use the remaining chart calculation of w divided by v. using our sample panel data, 60 watts divided by 12 volts equals 5 amps.

explanation:

answer:

// here is code in C++.

#include <bits/stdc++.h>

using namespace std;

//main function

int main()

{

  // variable

 int n;

 cout<<"enter a number:";

 // read the input

 cin>>n;

 // find the square root of the absolute value

 float square_root=sqrt(abs(n));

 // print the square_root

 cout<<"square root of "<<n<<" is: "<<square_root<<endl;

  return 0;

}

Explanation:

Read a number from user and assign it to "n".Then find its absolute value with abs() function.Then calculate the square root of the absolute value with sqrt() function.Print the square root of the number.

Output:

enter a number:-17

square root of -17 is: 4.12311

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                                                     sinserly Natalie 7 grader (this is not that hard)