Power Available for Reciprocating Engine-Propeller Combination Solution

STEP 0: Pre-Calculation Summary
Formula Used
Available Power = Propeller Efficiency*Brake Power
PA = η*BP
This formula uses 3 Variables
Variables Used
Available Power - (Measured in Watt) - Available Power is the power of the engine. It is a characteristic of the power plant and written in the manufacturer specifications of the engine.
Propeller Efficiency - Propeller Efficiency is defined as power produced (propeller power) divided by power applied (engine power).
Brake Power - (Measured in Watt) - Brake Power is the power available at the crankshaft.
STEP 1: Convert Input(s) to Base Unit
Propeller Efficiency: 0.93 --> No Conversion Required
Brake Power: 22.21 Watt --> 22.21 Watt No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
PA = η*BP --> 0.93*22.21
Evaluating ... ...
PA = 20.6553
STEP 3: Convert Result to Output's Unit
20.6553 Watt --> No Conversion Required
FINAL ANSWER
20.6553 Watt <-- Available Power
(Calculation completed in 00.004 seconds)

Credits

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Created by Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
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Verified by Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
Maiarutselvan V has verified this Calculator and 300+ more calculators!

Propeller Driven Airplane Calculators

Specific Fuel Consumption for given Range of Propeller-Driven Airplane
​ LaTeX ​ Go Specific Fuel Consumption = (Propeller Efficiency/Range of Propeller Aircraft)*(Lift Coefficient/Drag Coefficient)*(ln(Gross Weight/Weight without Fuel))
Range of Propeller-Driven Airplane
​ LaTeX ​ Go Range of Propeller Aircraft = (Propeller Efficiency/Specific Fuel Consumption)*(Lift Coefficient/Drag Coefficient)*(ln(Gross Weight/Weight without Fuel))
Propeller Efficiency for given Range of Propeller-Driven Airplane
​ LaTeX ​ Go Propeller Efficiency = Range of Propeller Aircraft*Specific Fuel Consumption*Drag Coefficient/(Lift Coefficient*ln(Gross Weight/Weight without Fuel))
Range of Propeller-Driven Airplane for given lift-to-drag ratio
​ LaTeX ​ Go Range of Propeller Aircraft = (Propeller Efficiency/Specific Fuel Consumption)*(Lift-to-Drag Ratio)*(ln(Gross Weight/Weight without Fuel))

Power Available for Reciprocating Engine-Propeller Combination Formula

​LaTeX ​Go
Available Power = Propeller Efficiency*Brake Power
PA = η*BP

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, Power Available for Reciprocating Engine-Propeller Combination is a measure of the effective power delivered by a reciprocating engine to a propeller, taking into account the propeller's efficiency and the engine's brake power. Available Power 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) & 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 -> 20.6553 = 0.93*22.21.

FAQ

What is Power Available for Reciprocating Engine-Propeller Combination?
Power Available for Reciprocating Engine-Propeller Combination is a measure of the effective power delivered by a reciprocating engine to a propeller, taking into account the propeller's efficiency and the engine's 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) & Brake Power is the power available at the crankshaft.
How to calculate Power Available for Reciprocating Engine-Propeller Combination?
Power Available for Reciprocating Engine-Propeller Combination is a measure of the effective power delivered by a reciprocating engine to a propeller, taking into account the propeller's efficiency and the engine's 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) & Brake Power (BP). With our tool, you need to enter the respective value for Propeller Efficiency & 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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