Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane Calculator

Category	Physics ↺
Physics	Flight Stability and Control ↺
Flight-Stability-And-Control	Airplane Performance ↺
Airplane-Performance	Range and Endurance of Jet Airplane ↺

✖Endurance of aircraft is the maximum length of time that an aircraft can spend in cruising flightⓘ Endurance of aircraft [E]			+10% -10%
✖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ⓘ Lift-to-drag ratio [L/D]			+10% -10%
✖The Gross Weight of the airplane is the weight with full fuel and payloadⓘ Gross Weight [W₀]			+10% -10%
✖Weight without fuel is the total weight of the airplane without fuelⓘ Weight without fuel [W₁]			+10% -10%

✖Thrust-specific fuel consumption (TSFC) is the fuel efficiency of an engine design with respect to thrust outputⓘ Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane [c_t]

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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

< 3 Other formulas that calculate the same Output

Thrust-Specific Fuel Consumption for given Range of Jet Airplane

Thrust-Specific Fuel Consumption=(sqrt(8/(Freestream density*Reference Area)))*(1/(Range of aircraft*Drag Coefficient))*(sqrt(lift coefficient))*((sqrt(Gross Weight))-(sqrt(Weight without fuel))) GO

Thrust-Specific Fuel Consumption for given Endurance of Jet Airplane

Thrust-Specific Fuel Consumption=lift coefficient*(ln(Gross Weight/Weight without fuel))/(Drag Coefficient*Endurance of aircraft) GO

Thrust specific fuel consumption

Thrust-Specific Fuel Consumption=(3600*Fuel air ratio)/Specific thrust GO

Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane Formula

Thrust-Specific Fuel Consumption=(1/Endurance of aircraft)*Lift-to-drag ratio*ln(Gross Weight/Weight without fuel)
ct=(1/E)*L/D*ln(W0/W1)

More formulas

Endurance of Jet Airplane GO

Thrust-Specific Fuel Consumption for given Endurance of Jet Airplane GO

Endurance for given 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

How to calculate fuel endurance?

The amount of fuel needed for a given flight can be calculated by multiplying the estimated flight time by the rate of consumption of fuel.

How to Calculate Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane?

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

How to calculate Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane using this online calculator? To use this online calculator for Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane, enter Endurance of aircraft (E), Lift-to-drag ratio (L/D), Gross Weight (W₀) and Weight without fuel (W₁) and hit the calculate button. Here is how the Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane calculation can be explained with given input values -> 0.001949 = (1/2000)*37*ln(5000/4500).

FAQ

What is Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane?

The Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane is a function of fuel weight and is represented as c_t=(1/E)*L/D*ln(W₀/W₁) or Thrust-Specific Fuel Consumption=(1/Endurance of aircraft)*Lift-to-drag ratio*ln(Gross Weight/Weight without fuel). Endurance of aircraft is the maximum length of time that an aircraft can spend in cruising flight, 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 Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane?

The Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane is a function of fuel weight is calculated using Thrust-Specific Fuel Consumption=(1/Endurance of aircraft)*Lift-to-drag ratio*ln(Gross Weight/Weight without fuel). To calculate Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane, you need Endurance of aircraft (E), 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 Endurance of aircraft, 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 Thrust-Specific Fuel Consumption?

In this formula, Thrust-Specific Fuel Consumption uses Endurance of aircraft, Lift-to-drag ratio, Gross Weight and Weight without fuel. We can use 3 other way(s) to calculate the same, which is/are as follows -

Thrust-Specific Fuel Consumption=(3600*Fuel air ratio)/Specific thrust
Thrust-Specific Fuel Consumption=lift coefficient*(ln(Gross Weight/Weight without fuel))/(Drag Coefficient*Endurance of aircraft)
Thrust-Specific Fuel Consumption=(sqrt(8/(Freestream density*Reference Area)))*(1/(Range of aircraft*Drag Coefficient))*(sqrt(lift coefficient))*((sqrt(Gross Weight))-(sqrt(Weight without fuel)))

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