Empty Weight Fraction Solution

STEP 0: Pre-Calculation Summary
Formula Used
Empty Weight Fraction = Operating Empty Weight/Desired Takeoff Weight
Ef = OEW/DTW
This formula uses 3 Variables
Variables Used
Empty Weight Fraction - Empty Weight Fraction is the ratio of the operating empty weight to the desired takeoff weight.
Operating Empty Weight - (Measured in Kilogram) - Operating Empty Weight of the aircraft is the aircraft's weight without including passengers, baggage, or fuel.
Desired Takeoff Weight - (Measured in Kilogram) - Desired Takeoff Weight (or mass) is the weight of the aircraft.
STEP 1: Convert Input(s) to Base Unit
Operating Empty Weight: 125000 Kilogram --> 125000 Kilogram No Conversion Required
Desired Takeoff Weight: 250000 Kilogram --> 250000 Kilogram No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Ef = OEW/DTW --> 125000/250000
Evaluating ... ...
Ef = 0.5
STEP 3: Convert Result to Output's Unit
0.5 --> No Conversion Required
FINAL ANSWER
0.5 <-- Empty Weight Fraction
(Calculation completed in 00.004 seconds)

Credits

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Created by Vedant Chitte
All India Shri Shivaji Memorials Society's ,College of Engineering (AISSMS COE PUNE), Pune
Vedant Chitte has created this Calculator and 25+ more calculators!
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Verified by Ravi Khiyani
Shri Govindram Seksaria Institute of Technology and Science (SGSITS), Indore
Ravi Khiyani has verified this Calculator and 300+ more calculators!

Preliminary Design Calculators

Optimum Range for Jet Aircraft in Cruising Phase
​ LaTeX ​ Go Range of Aircraft = (Velocity at Maximum Lift to Drag Ratio*Maximum Lift-to-Drag Ratio of Aircraft)/Power Specific Fuel Consumption*ln(Weight of Aircraft at Beginning of Cruise Phase/Weight of Aircraft at End of Cruise Phase)
Preliminary Take Off Weight Built-up for Manned Aircraft
​ LaTeX ​ Go Desired Takeoff Weight = Payload Carried+Operating Empty Weight+Fuel Weight to be Carried+Crew Weight
Preliminary Take off Weight Built-Up for Manned Aircraft given Fuel and Empty Weight Fraction
​ LaTeX ​ Go Desired Takeoff Weight = (Payload Carried+Crew Weight)/(1-Fuel Fraction-Empty Weight Fraction)
Fuel Fraction
​ LaTeX ​ Go Fuel Fraction = Fuel Weight to be Carried/Desired Takeoff Weight

Empty Weight Fraction Formula

​LaTeX ​Go
Empty Weight Fraction = Operating Empty Weight/Desired Takeoff Weight
Ef = OEW/DTW

What is empty weight of an aircraft?

The empty weight of an aircraft is the weight of the aircraft without including passengers, baggage, or fuel. Standard empty weight usually includes unusable fuel, full operating fluids, and full engine oil.

How to Calculate Empty Weight Fraction?

Empty Weight Fraction calculator uses Empty Weight Fraction = Operating Empty Weight/Desired Takeoff Weight to calculate the Empty Weight Fraction, The Empty Weight Fraction (EWF) is a parameter used in aircraft design and performance calculations to represent the ratio of the empty weight of the aircraft to its maximum takeoff weight (MTOW), it provides insights into the structural efficiency and payload-carrying capacity of the aircraft. Empty Weight Fraction is denoted by Ef symbol.

How to calculate Empty Weight Fraction using this online calculator? To use this online calculator for Empty Weight Fraction, enter Operating Empty Weight (OEW) & Desired Takeoff Weight (DTW) and hit the calculate button. Here is how the Empty Weight Fraction calculation can be explained with given input values -> 0.04 = 125000/250000.

FAQ

What is Empty Weight Fraction?
The Empty Weight Fraction (EWF) is a parameter used in aircraft design and performance calculations to represent the ratio of the empty weight of the aircraft to its maximum takeoff weight (MTOW), it provides insights into the structural efficiency and payload-carrying capacity of the aircraft and is represented as Ef = OEW/DTW or Empty Weight Fraction = Operating Empty Weight/Desired Takeoff Weight. Operating Empty Weight of the aircraft is the aircraft's weight without including passengers, baggage, or fuel & Desired Takeoff Weight (or mass) is the weight of the aircraft.
How to calculate Empty Weight Fraction?
The Empty Weight Fraction (EWF) is a parameter used in aircraft design and performance calculations to represent the ratio of the empty weight of the aircraft to its maximum takeoff weight (MTOW), it provides insights into the structural efficiency and payload-carrying capacity of the aircraft is calculated using Empty Weight Fraction = Operating Empty Weight/Desired Takeoff Weight. To calculate Empty Weight Fraction, you need Operating Empty Weight (OEW) & Desired Takeoff Weight (DTW). With our tool, you need to enter the respective value for Operating Empty Weight & Desired Takeoff Weight 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 Empty Weight Fraction?
In this formula, Empty Weight Fraction uses Operating Empty Weight & Desired Takeoff Weight. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Empty Weight Fraction = 1-Fuel Fraction-(Payload Carried+Crew Weight)/Desired Takeoff Weight
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