Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 200+ more calculators!
Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
Maiarutselvan V has verified this Calculator and 200+ more calculators!

11 Other formulas that you can solve using the same Inputs

Drag Coefficient for given zero-lift drag coefficient
Drag Coefficient=Zero-lift drag coefficient+((lift coefficient^2)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)) GO
Drag Coefficient for given parasite drag coefficient
Drag Coefficient=Parasite Drag coefficient+((lift coefficient^2)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)) GO
Coefficient of Drag due to lift
Coefficient of drag due to lift=(lift coefficient^2)/(pi*Oswald efficiency factor*Aspect Ratio of a wing) GO
Parasite Drag Coefficient at zero lift
Zero-lift drag coefficient=Drag Coefficient-Coefficient of drag due to lift GO
Thrust required for level, unaccelerated flight
Thrust of an aircraft=Dynamic Pressure*Area*Drag Coefficient GO
Dynamic pressure based on coefficient of lift
Dynamic Pressure=Lift force/(lift coefficient*Area) GO
Dynamic pressure
Dynamic Pressure=Drag Force/(Drag Coefficient*Area) GO
Drag for a level, unaccelerated flight at negligible thrust angle
Drag Force=Dynamic Pressure*Area*Drag Coefficient GO
Lift for a level, unaccelerated flight at negligible thrust angle
Lift force=Dynamic Pressure*Area*lift coefficient GO
Lift Force
Lift force=lift coefficient*Dynamic Pressure*Area GO
Drag force
Drag Force=Drag Coefficient*Dynamic Pressure*Area GO

5 Other formulas that calculate the same Output

Propeller Efficiency for given Endurance of Propeller-Driven Airplane
Propeller efficiency=Endurance of aircraft/((1/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
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
Propeller efficiency if thrust is known
Propeller efficiency=(Thrust*Aircraft forward speed)/Shaft power GO
Propeller efficiency for reciprocating engine-propeller combination
Propeller efficiency=Available Power/Brake power GO
Propeller Efficiency
Propeller efficiency=Thrust power/Shaft power GO

Propeller Efficiency for given Range of Propeller-Driven Airplane Formula

Propeller efficiency=Range of aircraft*Specific Fuel Consumption*Drag Coefficient/(lift coefficient*ln(Gross Weight/Weight without fuel))
η=R*c*C<sub>D</sub>/(C<sub>L</sub>*ln(W<sub>0</sub>/W<sub>1</sub>))
More formulas
Range of Propeller-Driven Airplane GO
Specific Fuel Consumption for given Range of Propeller-Driven Airplane GO
Range of Propeller-Driven Airplane for given lift-to-drag ratio GO
Propeller Efficiency for given Range and lift-to-drag ratio of Propeller-Driven Airplane GO
Specific Fuel Consumption for given Range and lift-to-drag ratio of Propeller-Driven Airplane GO
Lift-to-Drag ratio for given Range of Propeller-Driven Airplane GO
Endurance of Propeller-Driven Airplane GO
Propeller Efficiency for given Endurance of Propeller-Driven Airplane GO
Specific Fuel Consumption for given Endurance of Propeller-Driven Airplane GO

What is meant by the maximal total range of aircraft?

The maximal total range is the maximum distance an aircraft can fly between takeoff and landing, as limited by fuel capacity in powered aircraft, or cross-country speed and environmental conditions in unpowered aircraft.

How to Calculate Propeller Efficiency for given Range of Propeller-Driven Airplane?

Propeller Efficiency for given Range of Propeller-Driven Airplane calculator uses Propeller efficiency=Range of aircraft*Specific Fuel Consumption*Drag Coefficient/(lift coefficient*ln(Gross Weight/Weight without fuel)) to calculate the Propeller efficiency, The Propeller Efficiency for given Range of Propeller-Driven Airplane is a function of specific fuel consumption, aerodynamic coefficients, gross weight, and the weight without fuel of aircraft. Propeller efficiency and is denoted by η symbol.

How to calculate Propeller Efficiency for given Range of Propeller-Driven Airplane using this online calculator? To use this online calculator for Propeller Efficiency for given Range of Propeller-Driven Airplane, enter Range of aircraft (R), Specific Fuel Consumption (c), Drag Coefficient (CD), lift coefficient (CL), Gross Weight (W0) and Weight without fuel (W1) and hit the calculate button. Here is how the Propeller Efficiency for given Range of Propeller-Driven Airplane calculation can be explained with given input values -> 5.695E+6 = 100000*0.6*100/(10*ln(5000/4500)).

FAQ

What is Propeller Efficiency for given Range of Propeller-Driven Airplane?
The Propeller Efficiency for given Range of Propeller-Driven Airplane is a function of specific fuel consumption, aerodynamic coefficients, gross weight, and the weight without fuel of aircraft and is represented as η=R*c*CD/(CL*ln(W0/W1)) or Propeller efficiency=Range of aircraft*Specific Fuel Consumption*Drag Coefficient/(lift coefficient*ln(Gross Weight/Weight without fuel)). Range of aircraft is defined as the total distance (measured with respect to ground) traversed by the aircraft on a tank of fuel, Specific Fuel Consumption is a characteristic of the engine and defined as the weight of fuel consumed per unit power per unit time, 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, The lift coefficient (CL) 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. , 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 Propeller Efficiency for given Range of Propeller-Driven Airplane?
The Propeller Efficiency for given Range of Propeller-Driven Airplane is a function of specific fuel consumption, aerodynamic coefficients, gross weight, and the weight without fuel of aircraft is calculated using Propeller efficiency=Range of aircraft*Specific Fuel Consumption*Drag Coefficient/(lift coefficient*ln(Gross Weight/Weight without fuel)). To calculate Propeller Efficiency for given Range of Propeller-Driven Airplane, you need Range of aircraft (R), Specific Fuel Consumption (c), Drag Coefficient (CD), lift coefficient (CL), Gross Weight (W0) and Weight without fuel (W1). With our tool, you need to enter the respective value for Range of aircraft, Specific Fuel Consumption, Drag Coefficient, lift coefficient, 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 Propeller efficiency?
In this formula, Propeller efficiency uses Range of aircraft, Specific Fuel Consumption, Drag Coefficient, lift coefficient, Gross Weight and Weight without fuel. We can use 5 other way(s) to calculate the same, which is/are as follows -
  • Propeller efficiency=Thrust power/Shaft power
  • Propeller efficiency=Available Power/Brake power
  • Propeller efficiency=Range of aircraft*Specific Fuel Consumption/(Lift-to-drag ratio*(ln(Gross Weight/Weight without fuel)))
  • Propeller efficiency=Endurance of aircraft/((1/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))))
  • Propeller efficiency=(Thrust*Aircraft forward speed)/Shaft power
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