Matias Saibene
Development hell
Dear friends of the Orbiter forum.
Once again I am determined to move forward and not give up despite the problems I encounter in the development of my add-ons. However, I encounter the same problem again in the development of my latest creation (KleinVision's AirCar). As well as in the development of the XB-70 Valkyrie.
So far my latest flying creation, the I.Ae 37 works like a miracle because I barely touched the values of the VLiftCoeff function. However, I realize that I implemented it wrong.
The problem is not knowing how to adapt/program/or create a function that calculates the vertical or horizontal lift.
That's why I make this thread to ask for help in the particular cases that I have to do these functions to see if they can help me by correcting code, or suggesting ideas. Everything and everyone is welcome.
I apologize in advance for my ignorance, since I do not have high education, but I will try my best to implement the ideas you give me.
Or maybe there is a more "universal" way to do those VLiftCoeff and HLiftCoeff functions.
Next are the questions...
Once again I am determined to move forward and not give up despite the problems I encounter in the development of my add-ons. However, I encounter the same problem again in the development of my latest creation (KleinVision's AirCar). As well as in the development of the XB-70 Valkyrie.
So far my latest flying creation, the I.Ae 37 works like a miracle because I barely touched the values of the VLiftCoeff function. However, I realize that I implemented it wrong.
The problem is not knowing how to adapt/program/or create a function that calculates the vertical or horizontal lift.
That's why I make this thread to ask for help in the particular cases that I have to do these functions to see if they can help me by correcting code, or suggesting ideas. Everything and everyone is welcome.
I apologize in advance for my ignorance, since I do not have high education, but I will try my best to implement the ideas you give me.
Or maybe there is a more "universal" way to do those VLiftCoeff and HLiftCoeff functions.
Next are the questions...