Dynamic Pressure Calculator

✖Drag Force is the resisting force experienced by an object moving through a fluid.ⓘ Drag Force [F_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.ⓘ Drag Coefficient [C_D]			+10% -10%
✖Area for flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.ⓘ Area for Flow [A]			+10% -10%

✖Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.ⓘ Dynamic Pressure [q]

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Dynamic Pressure Solution

STEP 0: Pre-Calculation Summary

Formula Used

Dynamic Pressure = Drag Force/(Drag Coefficient*Area for Flow)
q = F_D/(C_D*A)
This formula uses 4 Variables

Variables Used

Dynamic Pressure - (Measured in Pascal) - Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.
Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid.
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.
Area for Flow - (Measured in Square Meter) - Area for flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.

STEP 1: Convert Input(s) to Base Unit

Drag Force: 80 Newton --> 80 Newton No Conversion Required
Drag Coefficient: 30 --> No Conversion Required
Area for Flow: 50 Square Meter --> 50 Square Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

q = F_D/(C_D*A) --> 80/(30*50)

Evaluating ... ...

q = 0.0533333333333333

STEP 3: Convert Result to Output's Unit

0.0533333333333333 Pascal --> No Conversion Required

FINAL ANSWER

0.0533333333333333 ≈ 0.053333 Pascal <-- Dynamic Pressure

(Calculation completed in 00.004 seconds)

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Credits

Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has created this Calculator and 300+ more calculators!

Verified by Rushi Shah

K J Somaiya College of Engineering (K J Somaiya), Mumbai

Rushi Shah has verified this Calculator and 200+ more calculators!

< Hypersonic Flow Parameters Calculators

Coefficient of Pressure with Similarity Parameters

LaTeX Go Pressure Coefficient = 2*Flow Deflection angle^2*((Specific Heat Ratio+1)/4+sqrt(((Specific Heat Ratio+1)/4)^2+1/Hypersonic Similarity Parameter^2))

Deflection Angle

LaTeX Go Deflection Angle = 2/(Specific Heat Ratio-1)*(1/Mach Number ahead of shock-1/Mach Number behind shock)

Coefficient of Drag

LaTeX Go Drag Coefficient = Drag Force/(Dynamic Pressure*Area for Flow)

Axial Force Coefficient

LaTeX Go Coefficient of Force = Force/(Dynamic Pressure*Area for Flow)

Dynamic Pressure Formula

LaTeX Go

Dynamic Pressure = Drag Force/(Drag Coefficient*Area for Flow)
q = F_D/(C_D*A)

What is dynamic pressure?

Dynamic pressure is the kinetic energy per unit volume of a fluid. Dynamic pressure is in fact one of the terms of Bernoulli's equation, which can be derived from the conservation of energy for a fluid in motion

How to Calculate Dynamic Pressure?

Dynamic Pressure calculator uses Dynamic Pressure = Drag Force/(Drag Coefficient*Area for Flow) to calculate the Dynamic Pressure, Dynamic Pressure formula is defined as a measure of the pressure exerted by a fluid due to its motion, commonly used in hypersonic flow parameters to describe the pressure experienced by an object moving at high velocities. It is an important parameter in aerodynamics and aerospace engineering, helping to predict the behavior of fluids under extreme conditions. Dynamic Pressure is denoted by q symbol.

How to calculate Dynamic Pressure using this online calculator? To use this online calculator for Dynamic Pressure, enter Drag Force (F_D), Drag Coefficient (C_D) & Area for Flow (A) and hit the calculate button. Here is how the Dynamic Pressure calculation can be explained with given input values -> 0.053333 = 80/(30*50).

FAQ

What is Dynamic Pressure?

Dynamic Pressure formula is defined as a measure of the pressure exerted by a fluid due to its motion, commonly used in hypersonic flow parameters to describe the pressure experienced by an object moving at high velocities. It is an important parameter in aerodynamics and aerospace engineering, helping to predict the behavior of fluids under extreme conditions and is represented as q = F_D/(C_D*A) or Dynamic Pressure = Drag Force/(Drag Coefficient*Area for Flow). Drag Force is the resisting force experienced by an object moving through a fluid, 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 & Area for flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.

How to calculate Dynamic Pressure?

Dynamic Pressure formula is defined as a measure of the pressure exerted by a fluid due to its motion, commonly used in hypersonic flow parameters to describe the pressure experienced by an object moving at high velocities. It is an important parameter in aerodynamics and aerospace engineering, helping to predict the behavior of fluids under extreme conditions is calculated using Dynamic Pressure = Drag Force/(Drag Coefficient*Area for Flow). To calculate Dynamic Pressure, you need Drag Force (F_D), Drag Coefficient (C_D) & Area for Flow (A). With our tool, you need to enter the respective value for Drag Force, Drag Coefficient & Area for Flow 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 Dynamic Pressure?

In this formula, Dynamic Pressure uses Drag Force, Drag Coefficient & Area for Flow. We can use 1 other way(s) to calculate the same, which is/are as follows -

Dynamic Pressure = Lift Force/(Lift Coefficient*Area for Flow)

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