The lab exercise this week (Week 03) was to write a program to compute the wing loading value (WLV), defined as the weight of an airplane (in kg) divided by its wing area (in m^2). Airplanes with low wing loading values are easy to maneuver but uncomfortable. Airplanes with high wing loading values are more comfortable, but less maneuverable. In this exercise, an engineer is trying to design an aircraft with a WLV in the range 290.0 - 310.0, inclusive.
You're going to write a C++ program to help the engineer in their design work. The program will input two real numbers, the weight (in kg) followed by the wing area (in m^2), and then compute the WLV. If the WLV falls within the design range of 290.0 - 310.0, inclusive, the program outputs "design: good". However, if the WLV falls outside this range, the program outputs how the wing area should change to achieve a WLV of 300.0. Example: suppose the inputs are (denoting weight and wing area, respectively):
38000.0 124.5
In this case the WLV is 305.221, so the program outputs
WLV: 305.221 design: good
because the WLV falls with the design goal of 290.0 - 310.0, inclusive. Note there is one space following each ":", and each line should be followed by C++ endl. However, suppose the inputs are
32000.0 99.2
The WLV 322.581, which is too high --- and implies the wing is too small. So the program outputs
WLV: 322.581 design: increase wing area by 7.46667m^2
because the target wing area (TWA) for the given weight is 106.66667 (i.e. 32000.0/TWA = 300.0), and 106.66667 - 99.2 = 7.46667. Likewise, suppose the inputs are
28500.0 102.25
The WLV is 278.729, which is too low --- and implies the wing is too big. So the program outputs
WLV: 278.729 design: reduce wing area by -7.25m^2
because the target wing area (TWA) for the given weight is 95.0, and 95.0 - 102.25 = -7.25. Finally, if either of the inputs is negative, do not perform the computation and instead output 'invalid data!". This implies the program has exactly one output: either "invalid data!", or the wing loading value followed by design guidelines.
[ HINT: you have the equation for WLV. Compute the engineer’s target wing area based on the weight and desired WLV of 300.0. Then you’ll have what you need to compute the change in wing area. It's just one or two lines of C++ code to compute what you need. ]
Explanation::
Code in C++::
#include<iostream>
using namespace std;
int main(){
cout<<"________________________________"<<endl;
/**
* Two double variables named weight and wingArea are declared
below.
* weight stores the weight of the airplane in kg
* wingArea stores the wing area in m^2
*/
double weight,wingArea;
/**
* Below we prompt user to enter the weight and wingArea
*/
cout<<"Enter Weight::";
cin>>weight;
cout<<"Enter Wing Area::";
cin>>wingArea;
if(weight<0 || wingArea<0){
/**
* If either of the input is negative then we print "invalid
data!"
* and the program is over here
*/
cout<<"invalid data!"<<endl;
}else{
/**
* An double variable named WLV is declared and initialize using the
formula.
*/
double WLV=weight/wingArea;
/**
* Below two double variables are declared named newWingArea and
difference.
* newWingArea will store the value of division of weight/300
* difference will store the difference between new wing area and
old wing area.
*/
double newWingArea,difference;
/**
* Below we just print the WLV value.
*/
cout<<"WLV: "<<WLV<<endl;
/**
* Now if the WLV is out of range 290.0 - 310.0 then we need to
calculate
* newWingArea and difference as follows.
*/
if(WLV<290.0 || WLV>310.0){
newWingArea=weight/300.0;
difference=newWingArea-wingArea;
if(difference>=0){
cout<<"design: increase wing area by
"<<difference<<"m^2"<<endl;
}else{
cout<<"design: reduce wing area by
"<<difference<<"m^2"<<endl;
}
}else{
/**
* If WLV falls in range 290.0 to 310.0 then we print good
design.
*/
cout<<"design: good"<<endl;
}
}
cout<<"________________________________"<<endl;
return 0;
}
OUTPUT::
Test Case 1::
Test Case 2::
Test Case 3::
Test Case 4::
Please provide feedback!!
Thank You!!
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