Coefficient of Drag Equation using Energy Released from Blast Wave Calculator

✖Energy for Blast Wave is the amount of work done.ⓘ Energy for Blast Wave [E]			+10% -10%
✖Freestream Density is the mass per unit volume of air far upstream of an aerodynamic body at a given altitude.ⓘ Freestream Density [ρ_∞]			+10% -10%
✖The Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air.ⓘ Freestream Velocity [V_∞]			+10% -10%
✖Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.ⓘ Diameter [d]			+10% -10%

✖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 Equation using Energy Released from Blast Wave [C_D]

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Coefficient of Drag Equation using Energy Released from Blast Wave Solution

STEP 0: Pre-Calculation Summary

Formula Used

Drag Coefficient = Energy for Blast Wave/(0.5*Freestream Density*Freestream Velocity^2*Diameter)
C_D = E/(0.5*ρ_∞*V_∞^2*d)
This formula uses 5 Variables

Variables Used

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.
Energy for Blast Wave - (Measured in Joule) - Energy for Blast Wave is the amount of work done.
Freestream Density - (Measured in Kilogram per Cubic Meter) - Freestream Density is the mass per unit volume of air far upstream of an aerodynamic body at a given altitude.
Freestream Velocity - (Measured in Meter per Second) - The Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air.
Diameter - (Measured in Meter) - Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.

STEP 1: Convert Input(s) to Base Unit

Energy for Blast Wave: 1033 Kilojoule --> 1033000 Joule (Check conversion here)
Freestream Density: 412.2 Kilogram per Cubic Meter --> 412.2 Kilogram per Cubic Meter No Conversion Required
Freestream Velocity: 102 Meter per Second --> 102 Meter per Second No Conversion Required
Diameter: 2.425 Meter --> 2.425 Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_D = E/(0.5*ρ_∞*V_∞^2*d) --> 1033000/(0.5*412.2*102^2*2.425)

Evaluating ... ...

C_D = 0.198659914068106

STEP 3: Convert Result to Output's Unit

0.198659914068106 --> No Conversion Required

FINAL ANSWER

0.198659914068106 ≈ 0.19866 <-- Drag Coefficient

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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

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< Planar and Blunt Slab Blast Wave Calculators

Creation Pressure for Planar Blast Wave

LaTeX Go Pressure = [BoltZ]*Freestream Density*(Energy for Blast Wave/Freestream Density)^(2/3)*Time Required for Blast Wave^(-2/3)

Energy for Blast Wave

LaTeX Go Energy for Blast Wave = 0.5*Freestream Density*Freestream Velocity^2*Drag Coefficient*Area for Blast Wave

Radial Coordinate for Planar Blast Wave

LaTeX Go Radial Coordinate = (Energy for Blast Wave/Freestream Density)^(1/3)*Time Required for Blast Wave^(2/3)

Time Required for Blast Wave

LaTeX Go Time Required for Blast Wave = Distance from X-Axis/Freestream Velocity

Coefficient of Drag Equation using Energy Released from Blast Wave Formula

LaTeX Go

Drag Coefficient = Energy for Blast Wave/(0.5*Freestream Density*Freestream Velocity^2*Diameter)
C_D = E/(0.5*ρ_∞*V_∞^2*d)

What is a drag coefficient?

The drag coefficient is a number that aerodynamicists use to model all of the complex dependencies of shape, inclination, and flow conditions on aircraft drag

How to Calculate Coefficient of Drag Equation using Energy Released from Blast Wave?

Coefficient of Drag Equation using Energy Released from Blast Wave calculator uses Drag Coefficient = Energy for Blast Wave/(0.5*Freestream Density*Freestream Velocity^2*Diameter) to calculate the Drag Coefficient, Coefficient of Drag Equation using Energy Released from Blast Wave formula is defined as a measure of the drag force experienced by an object moving at hypersonic speeds, relating the energy released from a blast wave to the object's velocity and air density. Drag Coefficient is denoted by C_D symbol.

How to calculate Coefficient of Drag Equation using Energy Released from Blast Wave using this online calculator? To use this online calculator for Coefficient of Drag Equation using Energy Released from Blast Wave, enter Energy for Blast Wave (E), Freestream Density (ρ_∞), Freestream Velocity (V_∞) & Diameter (d) and hit the calculate button. Here is how the Coefficient of Drag Equation using Energy Released from Blast Wave calculation can be explained with given input values -> 0.19866 = 1033000/(0.5*412.2*102^2*2.425).

FAQ

What is Coefficient of Drag Equation using Energy Released from Blast Wave?

Coefficient of Drag Equation using Energy Released from Blast Wave formula is defined as a measure of the drag force experienced by an object moving at hypersonic speeds, relating the energy released from a blast wave to the object's velocity and air density and is represented as C_D = E/(0.5*ρ_∞*V_∞^2*d) or Drag Coefficient = Energy for Blast Wave/(0.5*Freestream Density*Freestream Velocity^2*Diameter). Energy for Blast Wave is the amount of work done, Freestream Density is the mass per unit volume of air far upstream of an aerodynamic body at a given altitude, The Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air & Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.

How to calculate Coefficient of Drag Equation using Energy Released from Blast Wave?

Coefficient of Drag Equation using Energy Released from Blast Wave formula is defined as a measure of the drag force experienced by an object moving at hypersonic speeds, relating the energy released from a blast wave to the object's velocity and air density is calculated using Drag Coefficient = Energy for Blast Wave/(0.5*Freestream Density*Freestream Velocity^2*Diameter). To calculate Coefficient of Drag Equation using Energy Released from Blast Wave, you need Energy for Blast Wave (E), Freestream Density (ρ_∞), Freestream Velocity (V_∞) & Diameter (d). With our tool, you need to enter the respective value for Energy for Blast Wave, Freestream Density, Freestream Velocity & Diameter 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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