Endurance of Propeller-Driven Airplane Formula

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Endurance of Propeller Aircraft is the maximum length of time that an aircraft can spend in cruising flight. Check FAQs
Eprop=ηcCL1.5CD2ρS((1W1)12-(1W0)12)
Eprop - Endurance of Propeller Aircraft?η - Propeller Efficiency?c - Specific Fuel Consumption?CL - Lift Coefficient?CD - Drag Coefficient?ρ - Freestream Density?S - Reference Area?W1 - Weight without Fuel?W0 - Gross Weight?

Endurance of Propeller-Driven Airplane Example

With values
With units
Only example

Here is how the Endurance of Propeller-Driven Airplane equation looks like with Values.

Here is how the Endurance of Propeller-Driven Airplane equation looks like with Units.

Here is how the Endurance of Propeller-Driven Airplane equation looks like.

454.2055Edit=0.93Edit0.6Edit5Edit1.52Edit21.225Edit5.11Edit((13000Edit)12-(15000Edit)12)
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Endurance of Propeller-Driven Airplane Solution

Follow our step by step solution on how to calculate Endurance of Propeller-Driven Airplane?

FIRST Step Consider the formula
Eprop=ηcCL1.5CD2ρS((1W1)12-(1W0)12)
Next Step Substitute values of Variables
Eprop=0.930.6kg/h/W51.5221.225kg/m³5.11((13000kg)12-(15000kg)12)
Next Step Convert Units
Eprop=0.930.0002kg/s/W51.5221.225kg/m³5.11((13000kg)12-(15000kg)12)
Next Step Prepare to Evaluate
Eprop=0.930.000251.5221.2255.11((13000)12-(15000)12)
Next Step Evaluate
Eprop=454.205515825231s
LAST Step Rounding Answer
Eprop=454.2055s

Endurance of Propeller-Driven Airplane Formula Elements

Variables
Functions
Endurance of Propeller Aircraft
Endurance of Propeller Aircraft is the maximum length of time that an aircraft can spend in cruising flight.
Symbol: Eprop
Measurement: TimeUnit: s
Note: Value should be greater than 0.
Propeller Efficiency
Propeller Efficiency is defined as power produced (propeller power) divided by power applied (engine power).
Symbol: η
Measurement: NAUnit: Unitless
Note: Value should be less than 1.
Specific Fuel Consumption
Specific Fuel Consumption is a characteristic of the engine and defined as the weight of fuel consumed per unit power per unit time.
Symbol: c
Measurement: Specific Fuel ConsumptionUnit: kg/h/W
Note: Value should be greater than 0.
Lift Coefficient
The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.
Symbol: CL
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Drag Coefficient
Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.
Symbol: CD
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Freestream Density
Freestream Density is the mass per unit volume of air far upstream of an aerodynamic body at a given altitude.
Symbol: ρ
Measurement: DensityUnit: kg/m³
Note: Value can be positive or negative.
Reference Area
The Reference Area is arbitrarily an area that is characteristic of the object being considered. For an aircraft wing, the wing's planform area is called the reference wing area or simply wing area.
Symbol: S
Measurement: AreaUnit:
Note: Value should be greater than 0.
Weight without Fuel
Weight without Fuel is the total weight of the airplane without fuel.
Symbol: W1
Measurement: WeightUnit: kg
Note: Value should be greater than 0.
Gross Weight
The Gross Weight of the airplane is the weight with full fuel and payload.
Symbol: W0
Measurement: WeightUnit: kg
Note: Value should be greater than 0.
sqrt
A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.
Syntax: sqrt(Number)

Other formulas in Propeller Driven Airplane category

​Go Range of Propeller-Driven Airplane
Rprop=(ηc)(CLCD)(ln(W0W1))
​Go Propeller Efficiency for given Range of Propeller-Driven Airplane
η=RpropcCDCLln(W0W1)

How to Evaluate Endurance of Propeller-Driven Airplane?

Endurance of Propeller-Driven Airplane evaluator uses Endurance of Propeller Aircraft = Propeller Efficiency/Specific Fuel Consumption*(Lift Coefficient^1.5)/Drag Coefficient*sqrt(2*Freestream Density*Reference Area)*((1/Weight without Fuel)^(1/2)-(1/Gross Weight)^(1/2)) to evaluate the Endurance of Propeller Aircraft, Endurance of Propeller-Driven Airplane is a measure of the time an aircraft can stay aloft, which depends on factors such as propeller efficiency, specific fuel consumption, lift coefficient, drag coefficient, and aircraft weight. Endurance of Propeller Aircraft is denoted by Eprop symbol.

How to evaluate Endurance of Propeller-Driven Airplane using this online evaluator? To use this online evaluator for Endurance of Propeller-Driven Airplane, enter Propeller Efficiency (η), Specific Fuel Consumption (c), Lift Coefficient (CL), Drag Coefficient (CD), Freestream Density ), Reference Area (S), Weight without Fuel (W1) & Gross Weight (W0) and hit the calculate button.

FAQs on Endurance of Propeller-Driven Airplane

What is the formula to find Endurance of Propeller-Driven Airplane?
The formula of Endurance of Propeller-Driven Airplane is expressed as Endurance of Propeller Aircraft = Propeller Efficiency/Specific Fuel Consumption*(Lift Coefficient^1.5)/Drag Coefficient*sqrt(2*Freestream Density*Reference Area)*((1/Weight without Fuel)^(1/2)-(1/Gross Weight)^(1/2)). Here is an example- 454.2055 = 0.93/0.000166666666666667*(5^1.5)/2*sqrt(2*1.225*5.11)*((1/3000)^(1/2)-(1/5000)^(1/2)).
How to calculate Endurance of Propeller-Driven Airplane?
With Propeller Efficiency (η), Specific Fuel Consumption (c), Lift Coefficient (CL), Drag Coefficient (CD), Freestream Density ), Reference Area (S), Weight without Fuel (W1) & Gross Weight (W0) we can find Endurance of Propeller-Driven Airplane using the formula - Endurance of Propeller Aircraft = Propeller Efficiency/Specific Fuel Consumption*(Lift Coefficient^1.5)/Drag Coefficient*sqrt(2*Freestream Density*Reference Area)*((1/Weight without Fuel)^(1/2)-(1/Gross Weight)^(1/2)). This formula also uses Square Root Function function(s).
Can the Endurance of Propeller-Driven Airplane be negative?
No, the Endurance of Propeller-Driven Airplane, measured in Time cannot be negative.
Which unit is used to measure Endurance of Propeller-Driven Airplane?
Endurance of Propeller-Driven Airplane is usually measured using the Second[s] for Time. Millisecond[s], Microsecond[s], Nanosecond[s] are the few other units in which Endurance of Propeller-Driven Airplane can be measured.
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