Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 200+ more calculators!
Rushi Shah
K J Somaiya College of Engineering (K J Somaiya), Mumbai
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11 Other formulas that you can solve using the same Inputs

Diagonal of a Rectangle when breadth and area are given
Diagonal=sqrt(((Area)^2/(Breadth)^2)+(Breadth)^2) GO
Diagonal of a Rectangle when length and area are given
Diagonal=sqrt(((Area)^2/(Length)^2)+(Length)^2) GO
Side of a Kite when other side and area are given
Side A=(Area*cosec(Angle Between Sides))/Side B GO
Perimeter of rectangle when area and rectangle length are given
Perimeter=(2*Area+2*(Length)^2)/Length GO
Buoyant Force
Buoyant Force=Pressure*Area GO
Perimeter of a square when area is given
Perimeter=4*sqrt(Area) GO
Diagonal of a Square when area is given
Diagonal=sqrt(2*Area) GO
Length of rectangle when area and breadth are given
Length=Area/Breadth GO
Breadth of rectangle when area and length are given
Breadth=Area/Length GO
Pressure when force and area are given
Pressure=Force/Area GO
Stress
Stress=Force/Area GO

11 Other formulas that calculate the same Output

Drag Coefficient for given zero-lift drag coefficient
Drag Coefficient=Zero-lift drag coefficient+((lift coefficient^2)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)) GO
Drag Coefficient for given parasite drag coefficient
Drag Coefficient=Parasite Drag coefficient+((lift coefficient^2)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)) GO
Drag coefficient of flat plate laminar flow given Schmidt number
Drag Coefficient=(2*Convective mass transfer coefficient*(Schmidt Number^0.67))/Free stream velocity GO
Coefficient of drag equation using energy released from blast wave
Drag Coefficient=Energy/(0.5*Freestream density*(Freestream Velocity^2)*Diameter ) GO
Coefficient of Drag for given thrust and weight
Drag Coefficient=Thrust of an aircraft*lift coefficient/Weight GO
Coefficient of drag equation with coefficient of normal force
Drag Coefficient=coefficient of force*sin(Angle of attack) GO
Coefficient of Drag for given thrust-to-weight ratio
Drag Coefficient=lift coefficient*Thrust-to-weight ratio GO
Drag coefficient of flat plate in combined laminar turbulent flow
Drag Coefficient=0.0571/(Reynolds Number^0.2) GO
Drag coefficient of flat plate laminar flow
Drag Coefficient=0.644/(Reynolds Number^0.5) GO
Coefficient of drag equation with angle of attack
Drag Coefficient=2*(sin(Angle of attack))^3 GO
drag coefficient of flat plate laminar flow given friction factor
Drag Coefficient=Friction factor/4 GO

Coefficient of drag Formula

Drag Coefficient=Drag Force/(Dynamic Pressure*Area)
C<sub>D</sub>=F<sub>D</sub>/(P<sub>dynamic*A)
More formulas
Mach number GO
Dynamic pressure GO
lift coefficient GO
Lift Force GO
Drag force GO
Dynamic pressure based on coefficient of lift GO
Normal Force Coefficient GO
Deflection angle GO
Moment coefficient GO
Shear-stress distribution. GO
Axial force coefficient GO
Fourier’s law of heat conduction GO
Hypersonic similarity parameter GO
Coefficient of pressure with similarity parameters GO
Pressure ratio for high Mach number GO
Mach ratio at high mach number GO
Pressure ratio having high mach number with similarity constant GO
Newtonian sine-squared law for pressure coefficient GO
Supersonic expression for pressure coefficient on a surface with local deflection angle θ GO

What id coefficient of drag?.

In fluid dynamics, the 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

How to Calculate Coefficient of drag?

Coefficient of drag calculator uses Drag Coefficient=Drag Force/(Dynamic Pressure*Area) to calculate the Drag Coefficient, The coefficient of drag formula is defined as ratio of drag force acting on the body to the product of dynamic pressure and reference area. Drag Coefficient and is denoted by CD symbol.

How to calculate Coefficient of drag using this online calculator? To use this online calculator for Coefficient of drag, enter Drag Force (FD, Dynamic Pressure (Pdynamic) and Area (A) and hit the calculate button. Here is how the Coefficient of drag calculation can be explained with given input values -> 0.2 = 100/(10*50).

FAQ

What is Coefficient of drag?
The coefficient of drag formula is defined as ratio of drag force acting on the body to the product of dynamic pressure and reference area and is represented as CD=FDdynamic*A) or Drag Coefficient=Drag Force/(Dynamic Pressure*Area). Drag Force is the resisting force experienced by an object moving through a fluid, Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid and The area is the amount of two-dimensional space taken up by an object.
How to calculate Coefficient of drag?
The coefficient of drag formula is defined as ratio of drag force acting on the body to the product of dynamic pressure and reference area is calculated using Drag Coefficient=Drag Force/(Dynamic Pressure*Area). To calculate Coefficient of drag, you need Drag Force (FD, Dynamic Pressure (Pdynamic) and Area (A). With our tool, you need to enter the respective value for Drag Force, Dynamic Pressure and Area 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 Drag Coefficient?
In this formula, Drag Coefficient uses Drag Force, Dynamic Pressure and Area. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Drag Coefficient=Parasite Drag coefficient+((lift coefficient^2)/(pi*Oswald efficiency factor*Aspect Ratio of a wing))
  • Drag Coefficient=Zero-lift drag coefficient+((lift coefficient^2)/(pi*Oswald efficiency factor*Aspect Ratio of a wing))
  • Drag Coefficient=lift coefficient*Thrust-to-weight ratio
  • Drag Coefficient=Thrust of an aircraft*lift coefficient/Weight
  • Drag Coefficient=coefficient of force*sin(Angle of attack)
  • Drag Coefficient=2*(sin(Angle of attack))^3
  • Drag Coefficient=Energy/(0.5*Freestream density*(Freestream Velocity^2)*Diameter )
  • Drag Coefficient=0.644/(Reynolds Number^0.5)
  • Drag Coefficient=(2*Convective mass transfer coefficient*(Schmidt Number^0.67))/Free stream velocity
  • Drag Coefficient=Friction factor/4
  • Drag Coefficient=0.0571/(Reynolds Number^0.2)
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