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!

9 Other formulas that you can solve using the same Inputs

Specific Fuel Consumption for given Endurance of Propeller-Driven Airplane
Specific Fuel Consumption=(Propeller efficiency/Endurance of aircraft)*((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 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
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
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
Propeller efficiency for reciprocating engine-propeller combination
Propeller efficiency=Available Power/Brake power GO
Shaft brake power for reciprocating engine-propeller combination
Brake power=Available Power/Propeller efficiency GO

Power available for reciprocating engine-propeller combination Formula

Available Power=Propeller efficiency*Brake power
P<sub>A</sub>=η*BP
More formulas
Drag Coefficient for given parasite drag coefficient GO
Drag Coefficient for given zero-lift drag coefficient GO
Coefficient of Drag due to lift GO
Parasite Drag Coefficient at zero lift GO
Thrust in an accelerated flight GO
Drag in an accelerated flight GO
Lift in an accelerated flight GO
Centrifugal Force in an accelerated flight GO
Velocity in an accelerated flight GO
Thrust for a level, unaccelerated flight GO
Drag for a level, unaccelerated flight GO
Thrust angle for an unaccelerated flight for given drag GO
Lift for an unaccelerated flight GO
Weight of aircraft in level, unaccelerated flight GO
Thrust angle for an unaccelerated flight for given lift GO
Thrust required for level, unaccelerated flight GO
Drag for a level, unaccelerated flight at negligible thrust angle GO
Lift for a level, unaccelerated flight at negligible thrust angle GO
Weight of aircraft for a level, unaccelerated flight at negligible thrust angle GO
Thrust-to-weight ratio GO
Thrust for given coefficients of lift and drag GO
Weight of aircraft for given coefficients of lift and drag GO
Coefficient of Drag for given thrust-to-weight ratio GO
Coefficient of Lift for given thrust-to-weight ratio GO
Coefficient of Drag for given thrust and weight GO
Coefficient of Lift for given thrust and weight GO
Thrust required for given Lift-to-drag ratio GO
Weight of aircraft for given Lift-to-drag ratio GO
Lift-to-drag ratio for given required thrust GO
Minimum Thrust required GO
Zero-lift drag coefficient for given required thrust GO
Lift-induced drag coefficient for given required thrust GO
Minimum Thrust required for given lift coefficient GO
Zero-lift drag coefficient for given lift coefficient GO
Lift coefficient for given minimum required thrust GO
Minimum Thrust required for given weight GO
Zero-lift drag coefficient at minimum required thrust GO
Power required for given required thrust GO
Thrust required for given required power GO
Freestream velocity for given required power GO
Power required for given aerodynamic coefficients GO
Weight of aircraft for given required power GO
Zero-lift drag coefficient for minimum power required GO
Coefficient of Drag due to lift for minimum power required GO
Power required for given total drag GO
Total drag for given required power GO
Freestream Velocity for given total drag GO
Shaft brake power for reciprocating engine-propeller combination GO
Propeller efficiency for reciprocating engine-propeller combination GO
Rate of Climb GO
Velocity of aircraft at a given rate of climb GO
Flight path angle at a given rate of climb GO
Velocity at sea-level condition GO
Power required at sea-level condition GO
Velocity at an altitude GO
Power required at an altitude GO
Velocity at an altitude for given velocity at sea-level condition GO
Power required at an altitude for given power required at sea-level condition GO
Excess power GO
Thrust available for given excess power GO
Total Drag for given excess power GO
Velocity of aircraft for given excess power GO
Rate of Climb for given excess power GO
Excess power for given rate of climb GO
Weight of aircraft for given excess power GO
Glide angle GO
Glide angle for given lift-to-drag ratio GO
Lift-to-drag ratio for given glide angle GO
Lift for given glide angle GO
Drag for given glide angle GO
Range of Propeller-Driven Airplane GO
Propeller Efficiency for given 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
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
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
Resistance force during ground roll GO
Coefficient of rolling friction during ground roll GO
Weight of aircraft during ground roll GO
Lift acting on aircraft during ground roll GO
Ground effect factor GO
Drag during ground effect GO
Liftoff velocity for given stall velocity GO
Stall velocity for given liftoff velocity GO
Liftoff velocity for given weight GO
Stall velocity for given weight GO
Maximum Lift coefficient for given stall velocity GO
Maximum Lift coefficient for given liftoff velocity GO
Liftoff distance GO
Thrust for given liftoff distance GO
Lift during level turn GO
Bank angle during level turn GO
Weight during level turn GO
Load factor GO
Landing ground roll distance using thrust reversal GO
Touchdown velocity GO
Touchdown velocity for given stall velocity GO
Stall velocity for given touchdown velocity GO
Landing ground roll distance GO
Lift for a given load factor GO
Weight for a given load factor GO
Turn radius GO
Velocity for a given turn radius GO
Load factor for a given turn radius GO
Turn rate GO
Velocity for a given turn rate GO
Load factor for a given turn rate GO
Pull-up maneuver radius GO
Velocity for a given pull-up maneuver radius GO
Load factor for a given pull-up maneuver radius GO
Pull-up maneuver rate GO
Load factor for a given pull-up maneuver rate GO
Velocity for a given pull-up maneuver rate GO
Pull-down maneuver radius GO
Velocity for a given pull-down maneuver radius GO
Load factor for a given pull-down maneuver radius GO
Velocity for a given pull-down maneuver rate GO
Turn radius for a high load factor GO
Velocity for a given turn radius for a high load factor GO
Load factor for a given turn radius for a high-performance fighter aircraft GO
Load factor for a given turn rate for a high-performance fighter aircraft GO
Radius of turn for a given lift coefficient GO
Turn rate for a given lift coefficient GO
Lift Coefficient for a given turn rate GO
Radius of turn for a given wing loading GO
Lift Coefficient for a given wing loading and turn radius GO
Wing loading for a given turn radius GO
Turn rate for a given wing loading GO

What is the shaft power?

Shaft Power is the mechanical power transmitted from one rotating element of a vehicle, ship, and all types of machinery to another.

How to Calculate Power available for reciprocating engine-propeller combination?

Power available for reciprocating engine-propeller combination calculator uses Available Power=Propeller efficiency*Brake power to calculate the Available Power, The Power available for reciprocating engine-propeller combination is defined as the product of propeller efficiency and shaft brake power. Available Power and is denoted by PA symbol.

How to calculate Power available for reciprocating engine-propeller combination using this online calculator? To use this online calculator for Power available for reciprocating engine-propeller combination, enter Propeller efficiency (η) and Brake power (BP) and hit the calculate button. Here is how the Power available for reciprocating engine-propeller combination calculation can be explained with given input values -> 18.6 = 0.93*20.

FAQ

What is Power available for reciprocating engine-propeller combination?
The Power available for reciprocating engine-propeller combination is defined as the product of propeller efficiency and shaft brake power and is represented as PA=η*BP or Available Power=Propeller efficiency*Brake power. Propeller efficiency is defined as power produced (propeller power) divided by power applied (engine power) and Brake power is the power available at the crankshaft.
How to calculate Power available for reciprocating engine-propeller combination?
The Power available for reciprocating engine-propeller combination is defined as the product of propeller efficiency and shaft brake power is calculated using Available Power=Propeller efficiency*Brake power. To calculate Power available for reciprocating engine-propeller combination, you need Propeller efficiency (η) and Brake power (BP). With our tool, you need to enter the respective value for Propeller efficiency and Brake power and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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