The compressor inlet temperature for an ideal Brayton cycle is T_1 and the turbine inlet temperature is T_3. Using a cold air-standard analysis show that the temperature T_2 at the compressor exit that maximizes the net work developed per unit mass of air flow is T_2- (T_1 middot T_3)^1/2. draw two cycles at different temperatures T_2 and pressure ratio and identify the thermodynamic states points for the two cycles. Does T_4, the air temperature at the exit of the turbine, vary in between the two cycles?

answer:

walmart

explanation:

answer:

i am not 100% sure but i think it is a.)

dont take my word for it

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

                                                         This is easy

                                                     sinserly Natalie 7 grader (this is not that hard)

What is the MAIN responsibility of the President according to the Constitution? *