Dynamic pressure given drag coefficient Solution

STEP 0: Pre-Calculation Summary
Formula Used
Dynamic Pressure = Drag Force/Drag Coefficient
Pdynamic = 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) - 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 Newton --> 80 Newton No Conversion Required
Drag Coefficient: 30 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Pdynamic = FD/CD --> 80/30
Evaluating ... ...
Pdynamic = 2.66666666666667
STEP 3: Convert Result to Output's Unit
2.66666666666667 Pascal --> No Conversion Required
FINAL ANSWER
2.66666666666667 Pascal <-- Dynamic Pressure
(Calculation completed in 00.004 seconds)

Credits

Created by Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
Himanshu Sharma has created this Calculator and 50+ more calculators!
Verified by Kartikay Pandit
National Institute Of Technology (NIT), Hamirpur
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6 Dynamic Pressure Calculators

Dynamic pressure given gas constant

Dynamic pressure given gas constant

Formula
`"P"_{"dynamic"} = 1/2*"ρ"*"M"^2*"cp"*"R"*"T"`

Example
`"99960Pa"=1/2*"1.225kg/m³"*"8"^2*"3J/(kg*K)"*"10J/(kg*K)"*"85K"`

Calculator
LaTeX
Go Dynamic Pressure = 1/2*Ambient air density*Mach Number^2*Specific Heat of Air*Gas Constant*Temperature
Dynamic pressure given mach number

Dynamic pressure given mach number

Formula
`"P"_{"dynamic"} = 1/2*"ρ"*("M"*"a")^2`

Example
`"161400.6Pa"=1/2*"1.225kg/m³"*("8"*"231km/h")^2`

Calculator
LaTeX
Go Dynamic Pressure = 1/2*Ambient air density*(Mach Number*Sonic speed)^2
Dynamic pressure given normal pressure

Dynamic pressure given normal pressure

Formula
`"P"_{"dynamic"} = 1/2*"cp"*"p"*"M"^2`

Example
`"76800Pa"=1/2*"3J/(kg*K)"*"800Pa"*"8"^2`

Calculator
LaTeX
Go Dynamic Pressure = 1/2*Specific Heat of Air*Pressure*Mach Number^2
Dynamic pressure aircraft

Dynamic pressure aircraft

Formula
`"P"_{"dynamic"} = 1/2*"ρ"*("V"^2)`

Example
`"2124.09Pa"=1/2*"1.225kg/m³"*("212km/h"^2)`

Calculator
LaTeX
Go Dynamic Pressure = 1/2*Ambient air density*(Flight speed^2)
Dynamic pressure given lift coefficient

Dynamic pressure given lift coefficient

Formula
`"P"_{"dynamic"} = "L"/"C"_{"L"}`

Example
`"909.0909Pa"="1000N"/"1.1"`

Calculator
LaTeX
Go Dynamic Pressure = Lift Force/Lift Coefficient
Dynamic pressure given drag coefficient

Dynamic pressure given drag coefficient

Formula
`"P"_{"dynamic"} = "F"_{"D"}/"C"_{"D"}`

Example
`"2.666667Pa"="80N"/"30"`

Calculator
LaTeX
Go Dynamic Pressure = Drag Force/Drag Coefficient

Dynamic pressure given drag coefficient Formula

Dynamic Pressure = Drag Force/Drag Coefficient
Pdynamic = 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, The Dynamic pressure given drag coefficient formula is defined as pressure above ambient that develops when air is compressed and adiabatically brought to rest relative to the moving aircraft. Dynamic Pressure is denoted by Pdynamic 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 -> 2.666667 = 80/30.

FAQ

What is Dynamic pressure given drag coefficient?
The Dynamic pressure given drag coefficient formula is defined as pressure above ambient that develops when air is compressed and adiabatically brought to rest relative to the moving aircraft and is represented as Pdynamic = FD/CD or Dynamic Pressure = Drag Force/Drag Coefficient. 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?
The Dynamic pressure given drag coefficient formula is defined as pressure above ambient that develops when air is compressed and adiabatically brought to rest relative to the moving aircraft 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 5 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
  • Dynamic Pressure = 1/2*Ambient air density*Mach Number^2*Specific Heat of Air*Gas Constant*Temperature
  • Dynamic Pressure = 1/2*Specific Heat of Air*Pressure*Mach Number^2
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