Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft Solution

STEP 0: Pre-Calculation Summary
Formula Used
Maximum Lift-to-Drag Ratio = Lift to Drag Ratio at Maximum Endurance/0.866
LDmaxratio = LDEmaxratio/0.866
This formula uses 2 Variables
Variables Used
Maximum Lift-to-Drag Ratio - The Maximum Lift-to-Drag Ratio is the highest ratio of lift force to drag force that an aircraft can achieve.
Lift to Drag Ratio at Maximum Endurance - Lift to Drag Ratio at Maximum Endurance is the ratio of lift to drag at which the plane can fly (or loiter) for maximum time.
STEP 1: Convert Input(s) to Base Unit
Lift to Drag Ratio at Maximum Endurance: 4.4 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
LDmaxratio = LDEmaxratio/0.866 --> 4.4/0.866
Evaluating ... ...
LDmaxratio = 5.08083140877598
STEP 3: Convert Result to Output's Unit
5.08083140877598 --> No Conversion Required
FINAL ANSWER
5.08083140877598 5.080831 <-- Maximum Lift-to-Drag Ratio
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by Saurabh Patil
Shri Govindram Seksaria Institute of Technology and Science (SGSITS ), Indore
Saurabh Patil has created this Calculator and 700+ more calculators!
Verifier Image
Verified by Anshika Arya
National Institute Of Technology (NIT), Hamirpur
Anshika Arya has verified this Calculator and 2500+ 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))

Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft Formula

​LaTeX ​Go
Maximum Lift-to-Drag Ratio = Lift to Drag Ratio at Maximum Endurance/0.866
LDmaxratio = LDEmaxratio/0.866

What do you mean by Endurance of Aircraft?

In aviation, endurance is the maximum length of time that an aircraft can spend in cruising flight. In other words, it is the amount of time an aircraft can stay in the air with one load of fuel. Endurance is different from range, which is a measure of distance flown. For example, a typical sailplane exhibits high endurance characteristics but poor range characteristics. Endurance can factor into aviation design in a number of ways. Some aircraft, require high endurance characteristics as part of their mission profile (often referred to as loiter time). Endurance plays a prime factor in finding out the fuel fraction for an aircraft. Endurance, like range, is also related to fuel efficiency; fuel-efficient aircraft will tend to exhibit good endurance characteristics.

How to Calculate Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft?

Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft calculator uses Maximum Lift-to-Drag Ratio = Lift to Drag Ratio at Maximum Endurance/0.866 to calculate the Maximum Lift-to-Drag Ratio, Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft is a measure of the optimal aerodynamic efficiency of an aircraft propelled by a propeller, where the maximum endurance is achieved by maximizing the lift to drag ratio. Maximum Lift-to-Drag Ratio is denoted by LDmaxratio symbol.

How to calculate Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft using this online calculator? To use this online calculator for Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft, enter Lift to Drag Ratio at Maximum Endurance (LDEmaxratio) and hit the calculate button. Here is how the Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft calculation can be explained with given input values -> 98.15242 = 4.4/0.866.

FAQ

What is Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft?
Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft is a measure of the optimal aerodynamic efficiency of an aircraft propelled by a propeller, where the maximum endurance is achieved by maximizing the lift to drag ratio and is represented as LDmaxratio = LDEmaxratio/0.866 or Maximum Lift-to-Drag Ratio = Lift to Drag Ratio at Maximum Endurance/0.866. Lift to Drag Ratio at Maximum Endurance is the ratio of lift to drag at which the plane can fly (or loiter) for maximum time.
How to calculate Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft?
Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft is a measure of the optimal aerodynamic efficiency of an aircraft propelled by a propeller, where the maximum endurance is achieved by maximizing the lift to drag ratio is calculated using Maximum Lift-to-Drag Ratio = Lift to Drag Ratio at Maximum Endurance/0.866. To calculate Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft, you need Lift to Drag Ratio at Maximum Endurance (LDEmaxratio). With our tool, you need to enter the respective value for Lift to Drag Ratio at Maximum Endurance 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 Maximum Lift-to-Drag Ratio?
In this formula, Maximum Lift-to-Drag Ratio uses Lift to Drag Ratio at Maximum Endurance. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Maximum Lift-to-Drag Ratio = (Range of Propeller Aircraft*Specific Fuel Consumption)/(Propeller Efficiency*ln(Weight at Start of Cruise Phase/Weight at End of Cruise Phase))
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!