Coefficient of Drag due to Lift for Minimum Power required Calculator

✖Zero Lift Drag Coefficient is the coefficient of drag for an aircraft or aerodynamic body when it is producing zero lift.ⓘ Zero Lift Drag Coefficient [C_D,0]

+10%

-10%

✖The Coefficient of Drag Due to Lift represents the contribution of lift-induced drag to the total drag experienced by an aircraft.ⓘ Coefficient of Drag due to Lift for Minimum Power required [C_D,i]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Lift and Drag Requirements Formulas PDF PDF Image

Coefficient of Drag due to Lift for Minimum Power required Solution

STEP 0: Pre-Calculation Summary

Formula Used

Coefficient Of Drag Due to Lift = 3*Zero Lift Drag Coefficient
C_D,i = 3*C_D,0
This formula uses 2 Variables

Variables Used

Coefficient Of Drag Due to Lift - The Coefficient of Drag Due to Lift represents the contribution of lift-induced drag to the total drag experienced by an aircraft.
Zero Lift Drag Coefficient - Zero Lift Drag Coefficient is the coefficient of drag for an aircraft or aerodynamic body when it is producing zero lift.

STEP 1: Convert Input(s) to Base Unit

Zero Lift Drag Coefficient: 0.31 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_D,i = 3*C_D,0 --> 3*0.31

Evaluating ... ...

C_D,i = 0.93

STEP 3: Convert Result to Output's Unit

0.93 --> No Conversion Required

FINAL ANSWER

0.93 <-- Coefficient Of Drag Due to Lift

(Calculation completed in 00.004 seconds)

You are here -

Home » Physics » Aircraft Mechanics » Aircraft Performance » Level Flight » Aerospace » Lift and Drag Requirements » Coefficient of Drag due to Lift for Minimum Power required

Credits

Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

Vinay Mishra has created this Calculator and 300+ more calculators!

Verified by Sai Venkata Phanindra Chary Arendra

Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad

Sai Venkata Phanindra Chary Arendra has verified this Calculator and 300+ more calculators!

< Lift and Drag Requirements Calculators

Lift for Unaccelerated Flight

LaTeX Go Lift Force = Weight of Body-Thrust*sin(Thrust Angle)

Drag for Level and Unaccelerated Flight at Negligible Thrust Angle

LaTeX Go Drag Force = Dynamic Pressure*Area*Drag Coefficient

Lift for Level and Unaccelerated Flight at Negligible Thrust Angle

LaTeX Go Lift Force = Dynamic Pressure*Area*Lift Coefficient

Drag for Level and Unaccelerated Flight

LaTeX Go Drag Force = Thrust*cos(Thrust Angle)

Coefficient of Drag due to Lift for Minimum Power required Formula

LaTeX Go

Coefficient Of Drag Due to Lift = 3*Zero Lift Drag Coefficient
C_D,i = 3*C_D,0

What is a lift-induced drag?

Lift-induced drag, also known as induced drag, is a type of drag that occurs as a byproduct of generating lift by an airfoil (such as a wing or a blade). When an airfoil produces lift, it also creates vortices at its wingtips or blade tips. These vortices result in a downward deflection of air, which leads to a pressure difference between the upper and lower surfaces of the airfoil. This pressure difference generates a force called induced drag, which acts opposite to the direction of motion and is proportional to the lift produced.

How to Calculate Coefficient of Drag due to Lift for Minimum Power required?

Coefficient of Drag due to Lift for Minimum Power required calculator uses Coefficient Of Drag Due to Lift = 3*Zero Lift Drag Coefficient to calculate the Coefficient Of Drag Due to Lift, The Coefficient of Drag due to Lift for Minimum Power required is a dimensionless quantity that represents the aerodynamic drag resulting from the generation of lift. It calculates the coefficient of drag from the zero lift drag coefficient. Coefficient Of Drag Due to Lift is denoted by C_D,i symbol.

How to calculate Coefficient of Drag due to Lift for Minimum Power required using this online calculator? To use this online calculator for Coefficient of Drag due to Lift for Minimum Power required, enter Zero Lift Drag Coefficient (C_D,0) and hit the calculate button. Here is how the Coefficient of Drag due to Lift for Minimum Power required calculation can be explained with given input values -> 0.93 = 3*0.31.

FAQ

What is Coefficient of Drag due to Lift for Minimum Power required?

The Coefficient of Drag due to Lift for Minimum Power required is a dimensionless quantity that represents the aerodynamic drag resulting from the generation of lift. It calculates the coefficient of drag from the zero lift drag coefficient and is represented as C_D,i = 3*C_D,0 or Coefficient Of Drag Due to Lift = 3*Zero Lift Drag Coefficient. Zero Lift Drag Coefficient is the coefficient of drag for an aircraft or aerodynamic body when it is producing zero lift.

How to calculate Coefficient of Drag due to Lift for Minimum Power required?

The Coefficient of Drag due to Lift for Minimum Power required is a dimensionless quantity that represents the aerodynamic drag resulting from the generation of lift. It calculates the coefficient of drag from the zero lift drag coefficient is calculated using Coefficient Of Drag Due to Lift = 3*Zero Lift Drag Coefficient. To calculate Coefficient of Drag due to Lift for Minimum Power required, you need Zero Lift Drag Coefficient (C_D,0). With our tool, you need to enter the respective value for Zero Lift Drag Coefficient 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 Coefficient Of Drag Due to Lift?

In this formula, Coefficient Of Drag Due to Lift uses Zero Lift Drag Coefficient. We can use 1 other way(s) to calculate the same, which is/are as follows -

Coefficient Of Drag Due to Lift = (Thrust/(Dynamic Pressure*Reference Area))-Zero Lift Drag Coefficient

Home

FREE PDFs

🔍 Search