Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has verified this Calculator and 200+ more calculators!

11 Other formulas that you can solve using the same Inputs

Endurance of Propeller-Driven Airplane
Endurance of aircraft=(Propeller efficiency/Specific Fuel Consumption)*((lift coefficient^1.5)/Drag Coefficient)*(sqrt(2*Freestream density*Reference Area))*(((1/Gross Weight)^(1/2))-((1/Weight without fuel)^(1/2))) GO
Specific Fuel Consumption for given Range of Propeller-Driven Airplane
Specific Fuel Consumption=(Propeller efficiency/Range of aircraft)*(lift coefficient/Drag Coefficient)*(ln(Gross Weight/Weight without fuel)) GO
Range of Propeller-Driven Airplane
Range of aircraft=(Propeller efficiency/Specific Fuel Consumption)*(lift coefficient/Drag Coefficient)*(ln(Gross Weight/Weight without fuel)) GO
Propeller Efficiency for given Range of Propeller-Driven Airplane
Propeller efficiency=Range of aircraft*Specific Fuel Consumption*Drag Coefficient/(lift coefficient*ln(Gross Weight/Weight without fuel)) GO
Specific Fuel Consumption for given Range and lift-to-drag ratio of Propeller-Driven Airplane
Specific Fuel Consumption=(Propeller efficiency/Range of aircraft)*(Lift-to-drag ratio)*(ln(Gross Weight/Weight without fuel)) GO
Range of Propeller-Driven Airplane for given lift-to-drag ratio
Range of aircraft=(Propeller efficiency/Specific Fuel Consumption)*(Lift-to-drag ratio)*(ln(Gross Weight/Weight without fuel)) GO
Propeller Efficiency for given Range and lift-to-drag ratio of Propeller-Driven Airplane
Propeller efficiency=Range of aircraft*Specific Fuel Consumption/(Lift-to-drag ratio*(ln(Gross Weight/Weight without fuel))) GO
Lift-to-Drag ratio for given Range of Propeller-Driven Airplane
Lift-to-drag ratio=Specific Fuel Consumption*Range of aircraft/(Propeller efficiency*ln(Gross Weight/Weight without fuel)) GO
Weight of aircraft for given Lift-to-drag ratio
Weight=Thrust of an aircraft*Lift-to-drag ratio GO
Thrust required for given Lift-to-drag ratio
Thrust of an aircraft=Weight/Lift-to-drag ratio GO
Glide angle for given lift-to-drag ratio
Glide angle=atan(1/Lift-to-drag ratio) GO

2 Other formulas that calculate the same Output

Endurance of Propeller-Driven Airplane
Endurance of aircraft=(Propeller efficiency/Specific Fuel Consumption)*((lift coefficient^1.5)/Drag Coefficient)*(sqrt(2*Freestream density*Reference Area))*(((1/Gross Weight)^(1/2))-((1/Weight without fuel)^(1/2))) GO
Endurance of Jet Airplane
Endurance of aircraft=lift coefficient*(ln(Gross Weight/Weight without fuel))/(Drag Coefficient*Thrust-Specific Fuel Consumption) GO

Endurance for given Lift-to-Drag ratio of Jet Airplane Formula

Endurance of aircraft=(1/Thrust-Specific Fuel Consumption)*Lift-to-drag ratio*ln(Gross Weight/Weight without fuel)
E=(1/c<sub>t</sub>)*L/D*ln(W<sub>0</sub>/W<sub>1</sub>)
More formulas
Endurance of Jet Airplane GO
Thrust-Specific Fuel Consumption for given Endurance of Jet Airplane GO
Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane GO
Lift-to-Drag ratio for given Endurance of Jet Airplane GO
Range of Jet Airplane GO
Thrust-Specific Fuel Consumption for given Range of Jet Airplane GO

Which is the most fuel-efficient type of gas turbine engine?

The turbofan, with lower thrust-specific fuel consumption, is more fuel-efficient. The values of 1.0 for a turbojet and 0.5 for a turbofan are typical sea-level static values.

How to Calculate Endurance for given Lift-to-Drag ratio of Jet Airplane?

Endurance for given Lift-to-Drag ratio of Jet Airplane calculator uses Endurance of aircraft=(1/Thrust-Specific Fuel Consumption)*Lift-to-drag ratio*ln(Gross Weight/Weight without fuel) to calculate the Endurance of aircraft, The Endurance for given Lift-to-Drag ratio of Jet Airplane is a function of thrust specific fuel consumption and fuel weight. Endurance of aircraft and is denoted by E symbol.

How to calculate Endurance for given Lift-to-Drag ratio of Jet Airplane using this online calculator? To use this online calculator for Endurance for given Lift-to-Drag ratio of Jet Airplane, enter Thrust-Specific Fuel Consumption (ct), Lift-to-drag ratio (L/D), Gross Weight (W0) and Weight without fuel (W1) and hit the calculate button. Here is how the Endurance for given Lift-to-Drag ratio of Jet Airplane calculation can be explained with given input values -> 1.299446 = (1/3)*37*ln(5000/4500).

FAQ

What is Endurance for given Lift-to-Drag ratio of Jet Airplane?
The Endurance for given Lift-to-Drag ratio of Jet Airplane is a function of thrust specific fuel consumption and fuel weight and is represented as E=(1/ct)*L/D*ln(W0/W1) or Endurance of aircraft=(1/Thrust-Specific Fuel Consumption)*Lift-to-drag ratio*ln(Gross Weight/Weight without fuel). Thrust-specific fuel consumption (TSFC) is the fuel efficiency of an engine design with respect to thrust output, The Lift-to-drag ratio is the amount of lift generated by a wing or vehicle, divided by the aerodynamic drag it creates by moving through the air, The Gross Weight of the airplane is the weight with full fuel and payload and Weight without fuel is the total weight of the airplane without fuel.
How to calculate Endurance for given Lift-to-Drag ratio of Jet Airplane?
The Endurance for given Lift-to-Drag ratio of Jet Airplane is a function of thrust specific fuel consumption and fuel weight is calculated using Endurance of aircraft=(1/Thrust-Specific Fuel Consumption)*Lift-to-drag ratio*ln(Gross Weight/Weight without fuel). To calculate Endurance for given Lift-to-Drag ratio of Jet Airplane, you need Thrust-Specific Fuel Consumption (ct), Lift-to-drag ratio (L/D), Gross Weight (W0) and Weight without fuel (W1). With our tool, you need to enter the respective value for Thrust-Specific Fuel Consumption, Lift-to-drag ratio, Gross Weight and Weight without fuel and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Endurance of aircraft?
In this formula, Endurance of aircraft uses Thrust-Specific Fuel Consumption, Lift-to-drag ratio, Gross Weight and Weight without fuel. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Endurance of aircraft=(Propeller efficiency/Specific Fuel Consumption)*((lift coefficient^1.5)/Drag Coefficient)*(sqrt(2*Freestream density*Reference Area))*(((1/Gross Weight)^(1/2))-((1/Weight without fuel)^(1/2)))
  • Endurance of aircraft=lift coefficient*(ln(Gross Weight/Weight without fuel))/(Drag Coefficient*Thrust-Specific Fuel Consumption)
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