Range Of Propeller Engine Given By Lift-to-Drag Ratio Calculator

The range of a propeller engine refers to the maximum distance an aircraft can travel on a single tank of fuel without refueling. It is a critical performance parameter influenced by factors such as fuel efficiency, aircraft design, cruising speed, and payload capacity. The range of a propeller engine is vital for determining its operational capabilities and is a key consideration in aviation planning and decision-making. The formula to Calculate Range of Propeller Engine as follows:

Where:

  • is the propeller efficiency.
  •  is the specific fuel consumption kg/Ws
  •  is the Gross Weight in kg.
  •  is the Weight without fuel in kg.
  • R is the Range of Propeller Engine in m.
  • L/D is the Lift-to-Drag Ratio.

Leave a Comment

Your email address will not be published. Required fields are marked *

Scroll to Top