Parasite Drag Coefficient at zero lift Calculator

✖Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.ⓘ Drag Coefficient [C_D]			+10% -10%
✖The Coefficient of drag due to lift is the sum of the coefficients of induced drag and the increment in parasite drag due to the angle of attack different from the zero-lift angle of attack.ⓘ Coefficient of Drag due to Lift [C_D,i]			+10% -10%

✖The Zero-lift drag coefficient is a dimensionless parameter that relates an aircraft's zero-lift drag force to its size, speed, and flying altitude.ⓘ Parasite Drag Coefficient at zero lift [C_D,0]

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Parasite Drag Coefficient at zero lift Solution

STEP 0: Pre-Calculation Summary

Formula Used

Zero-Lift Drag Coefficient = Drag Coefficient-Coefficient of Drag due to Lift
C_D,0 = C_D-C_D,i
This formula uses 3 Variables

Variables Used

Zero-Lift Drag Coefficient - The Zero-lift drag coefficient is a dimensionless parameter that relates an aircraft's zero-lift drag force to its size, speed, and flying altitude.
Drag Coefficient - Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.
Coefficient of Drag due to Lift - The Coefficient of drag due to lift is the sum of the coefficients of induced drag and the increment in parasite drag due to the angle of attack different from the zero-lift angle of attack.

STEP 1: Convert Input(s) to Base Unit

Drag Coefficient: 30 --> No Conversion Required
Coefficient of Drag due to Lift: 0.19 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_D,0 = C_D-C_D,i --> 30-0.19

Evaluating ... ...

C_D,0 = 29.81

STEP 3: Convert Result to Output's Unit

29.81 --> No Conversion Required

FINAL ANSWER

29.81 <-- Zero-Lift Drag Coefficient

(Calculation completed in 00.004 seconds)

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Home » Physics » Aircraft Mechanics » Introduction and Governing Equations » Aerospace » Lift and Drag Polar » Parasite Drag Coefficient at zero lift

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Created by Vinay Mishra

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

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Institute of Aeronautical Engineering (IARE), Hyderabad

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< Lift and Drag Polar Calculators

Drag Coefficient for given zero-lift drag coefficient

LaTeX Go Drag Coefficient = Zero-Lift Drag Coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))

Drag Coefficient for given parasite drag coefficient

LaTeX Go Drag Coefficient = Parasite Drag coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))

Coefficient of Drag due to lift

LaTeX Go Coefficient of Drag due to Lift = (Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing)

Parasite Drag Coefficient at zero lift

LaTeX Go Zero-Lift Drag Coefficient = Drag Coefficient-Coefficient of Drag due to Lift

Parasite Drag Coefficient at zero lift Formula

LaTeX Go

Zero-Lift Drag Coefficient = Drag Coefficient-Coefficient of Drag due to Lift
C_D,0 = C_D-C_D,i

How do you stop a parasitic drag?

There are two ways to decrease friction drag: the first is to shape the moving body so that laminar flow is possible. The second method is to increase the length and decrease the cross-section of the moving object as much as practicable.

How to Calculate Parasite Drag Coefficient at zero lift?

Parasite Drag Coefficient at zero lift calculator uses Zero-Lift Drag Coefficient = Drag Coefficient-Coefficient of Drag due to Lift to calculate the Zero-Lift Drag Coefficient, Parasite Drag Coefficient at Zero Lift is a measure of the air resistance caused by the shape of an object, excluding the drag due to lift, which affects the object's motion through a fluid, such as air or water, at zero lift conditions. Zero-Lift Drag Coefficient is denoted by C_D,0 symbol.

How to calculate Parasite Drag Coefficient at zero lift using this online calculator? To use this online calculator for Parasite Drag Coefficient at zero lift, enter Drag Coefficient (C_D) & Coefficient of Drag due to Lift (C_D,i) and hit the calculate button. Here is how the Parasite Drag Coefficient at zero lift calculation can be explained with given input values -> 29.9 = 30-0.19.

FAQ

What is Parasite Drag Coefficient at zero lift?

Parasite Drag Coefficient at Zero Lift is a measure of the air resistance caused by the shape of an object, excluding the drag due to lift, which affects the object's motion through a fluid, such as air or water, at zero lift conditions and is represented as C_D,0 = C_D-C_D,i or Zero-Lift Drag Coefficient = Drag Coefficient-Coefficient of Drag due to Lift. Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water & The Coefficient of drag due to lift is the sum of the coefficients of induced drag and the increment in parasite drag due to the angle of attack different from the zero-lift angle of attack.

How to calculate Parasite Drag Coefficient at zero lift?

Parasite Drag Coefficient at Zero Lift is a measure of the air resistance caused by the shape of an object, excluding the drag due to lift, which affects the object's motion through a fluid, such as air or water, at zero lift conditions is calculated using Zero-Lift Drag Coefficient = Drag Coefficient-Coefficient of Drag due to Lift. To calculate Parasite Drag Coefficient at zero lift, you need Drag Coefficient (C_D) & Coefficient of Drag due to Lift (C_D,i). With our tool, you need to enter the respective value for Drag Coefficient & Coefficient of Drag due to Lift 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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