The CurvFitXYZ program can be a tool for fitting aircraft flight data for use in a mission program that predicts aircraft performance. The curve fit method provides a more accurate means of modeling flight data than table look-up procedures which use linear interpolation between data points.
Examples of some of the many performance flight parameters which lend themselves to good curve fits are as follows:
Climb
Time, Distance & Fuel to Climb = f (Drag Index, Altitude)
Normal Descent From a Given Altitude
Time, Distance & Fuel to Descend = f (Drag Index, Altitude)
Cruise at Constant Speed and Altitude
Specific Range = f (Gross Weight, Drag Index)
Optimum Cruise
Optimum Cruise Speed = f (Altitude, Gross Weight)
Alternate Cruise Curve Fit Method at Constant Speed
Fuel Flow at Base Weight & 0 Drag Index = f ( Altitude)
Delta Fuel Flow (weight sensitivity) = f (Gross Weight, Altitude)
Delta Fuel Flow (drag sensitivity) = f (Drag Index, Altitude)
Maximum Endurance at Constant Altitude
Specific Range = f (Gross Weight, Drag Index)