Dynamic Pressure given Drag Coefficient Solution

STEP 0: Pre-Calculation Summary
Formula Used
Dynamic Pressure = Drag Force/Drag Coefficient
q = FD/CD
This formula uses 3 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) - The 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.
STEP 1: Convert Input(s) to Base Unit
Drag Force: 80.05 Newton --> 80.05 Newton No Conversion Required
Drag Coefficient: 1.134 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
q = FD/CD --> 80.05/1.134
Evaluating ... ...
q = 70.5908289241623
STEP 3: Convert Result to Output's Unit
70.5908289241623 Pascal --> No Conversion Required
FINAL ANSWER
70.5908289241623 70.59083 Pascal <-- Dynamic Pressure
(Calculation completed in 00.006 seconds)

Credits

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Created by Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
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Verified by Kartikay Pandit
National Institute Of Technology (NIT), Hamirpur
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Preliminary Aerodynamics Calculators

Power required at sea-level conditions
​ LaTeX ​ Go Power Required at Sea-level = sqrt((2*Weight of Body^3*Drag Coefficient^2)/([Std-Air-Density-Sea]*Reference Area*Lift Coefficient^3))
Power required at Altitude
​ LaTeX ​ Go Power Required at Altitude = sqrt((2*Weight of Body^3*Drag Coefficient^2)/(Density*Reference Area*Lift Coefficient^3))
Velocity at Sea-Level given Lift Coefficient
​ LaTeX ​ Go Velocity at Sea-Level = sqrt((2*Weight of Body)/([Std-Air-Density-Sea]*Reference Area*Lift Coefficient))
Velocity at Altitude
​ LaTeX ​ Go Velocity at an Altitude = sqrt(2*Weight of Body/(Density*Reference Area*Lift Coefficient))

Dynamic Pressure given Drag Coefficient Formula

​LaTeX ​Go
Dynamic Pressure = Drag Force/Drag Coefficient
q = FD/CD

What is dynamic pressure?

It is the pressure on a surface at which a flowing fluid is brought to rest in excess of the pressure on it when the fluid is not flowing.

How to Calculate Dynamic Pressure given Drag Coefficient?

Dynamic Pressure given Drag Coefficient calculator uses Dynamic Pressure = Drag Force/Drag Coefficient to calculate the Dynamic Pressure, Dynamic Pressure given Drag Coefficient is a measure of the pressure exerted by a fluid, such as air or water, as it flows around an object, calculated by dividing the drag force by the drag coefficient, and is a fundamental concept in preliminary aerodynamics. Dynamic Pressure is denoted by q symbol.

How to calculate Dynamic Pressure given Drag Coefficient using this online calculator? To use this online calculator for Dynamic Pressure given Drag Coefficient, enter Drag Force (FD) & Drag Coefficient (CD) and hit the calculate button. Here is how the Dynamic Pressure given Drag Coefficient calculation can be explained with given input values -> 66.70833 = 80.05/1.134.

FAQ

What is Dynamic Pressure given Drag Coefficient?
Dynamic Pressure given Drag Coefficient is a measure of the pressure exerted by a fluid, such as air or water, as it flows around an object, calculated by dividing the drag force by the drag coefficient, and is a fundamental concept in preliminary aerodynamics and is represented as q = FD/CD or Dynamic Pressure = Drag Force/Drag Coefficient. The 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.
How to calculate Dynamic Pressure given Drag Coefficient?
Dynamic Pressure given Drag Coefficient is a measure of the pressure exerted by a fluid, such as air or water, as it flows around an object, calculated by dividing the drag force by the drag coefficient, and is a fundamental concept in preliminary aerodynamics is calculated using Dynamic Pressure = Drag Force/Drag Coefficient. To calculate Dynamic Pressure given Drag Coefficient, you need Drag Force (FD) & Drag Coefficient (CD). With our tool, you need to enter the respective value for Drag Force & 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 Dynamic Pressure?
In this formula, Dynamic Pressure uses Drag Force & Drag Coefficient. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Dynamic Pressure = Lift Force/Lift Coefficient
  • Dynamic Pressure = 1/2*Ambient Air Density*Flight Speed^2
  • Dynamic Pressure = 1/2*Ambient Air Density*(Mach Number*Sonic Speed)^2
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