How to Calculate Optimum Range for Jet Aircraft in Cruising Phase?
Optimum Range for Jet Aircraft in Cruising Phase calculator uses Range of Aircraft = (Velocity at Maximum Lift to Drag Ratio*Maximum Lift to Drag Ratio of Aircraft)/Power Specific Fuel Consumption*ln(Weight of Aircraft at Beginning of Cruise Phase/Weight of Aircraft at End of Cruise Phase) to calculate the Range of Aircraft, The Optimum Range for Jet Aircraft in Cruising Phase formula is defined as the maximum range of plane that can be traveled in phase of cruise. Range of Aircraft is denoted by R symbol.
How to calculate Optimum Range for Jet Aircraft in Cruising Phase using this online calculator? To use this online calculator for Optimum Range for Jet Aircraft in Cruising Phase, enter Velocity at Maximum Lift to Drag Ratio (VL/D(max)), Maximum Lift to Drag Ratio of Aircraft (LDmaxratio), Power Specific Fuel Consumption (c), Weight of Aircraft at Beginning of Cruise Phase (Wi) & Weight of Aircraft at End of Cruise Phase (Wf) and hit the calculate button. Here is how the Optimum Range for Jet Aircraft in Cruising Phase calculation can be explained with given input values -> 0.087269 = (1.92916666666667*30)/0.000166666666666667*ln(450/350).