Dynamic Pressure given Lift Coefficient Solution

STEP 0: Pre-Calculation Summary
Formula Used
Dynamic Pressure = Lift Force/Lift Coefficient
q = FL/CL
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.
Lift Force - (Measured in Newton) - The Lift Force, lifting force, or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of flow.
Lift Coefficient - The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.
STEP 1: Convert Input(s) to Base Unit
Lift Force: 20.45 Newton --> 20.45 Newton No Conversion Required
Lift Coefficient: 0.29 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
q = FL/CL --> 20.45/0.29
Evaluating ... ...
q = 70.5172413793103
STEP 3: Convert Result to Output's Unit
70.5172413793103 Pascal --> No Conversion Required
FINAL ANSWER
70.5172413793103 70.51724 Pascal <-- Dynamic Pressure
(Calculation completed in 00.020 seconds)

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Created by Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
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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 Lift Coefficient Formula

​LaTeX ​Go
Dynamic Pressure = Lift Force/Lift Coefficient
q = FL/CL

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 Lift Coefficient?

Dynamic Pressure given Lift Coefficient calculator uses Dynamic Pressure = Lift Force/Lift Coefficient to calculate the Dynamic Pressure, Dynamic Pressure given Lift Coefficient is a measure of the pressure exerted by a fluid, such as air or water, as it moves around an object, which is influenced by the lift force and lift coefficient. Dynamic Pressure is denoted by q symbol.

How to calculate Dynamic Pressure given Lift Coefficient using this online calculator? To use this online calculator for Dynamic Pressure given Lift Coefficient, enter Lift Force (FL) & Lift Coefficient (CL) and hit the calculate button. Here is how the Dynamic Pressure given Lift Coefficient calculation can be explained with given input values -> 70.65517 = 20.45/0.29.

FAQ

What is Dynamic Pressure given Lift Coefficient?
Dynamic Pressure given Lift Coefficient is a measure of the pressure exerted by a fluid, such as air or water, as it moves around an object, which is influenced by the lift force and lift coefficient and is represented as q = FL/CL or Dynamic Pressure = Lift Force/Lift Coefficient. The Lift Force, lifting force, or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of flow & The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.
How to calculate Dynamic Pressure given Lift Coefficient?
Dynamic Pressure given Lift Coefficient is a measure of the pressure exerted by a fluid, such as air or water, as it moves around an object, which is influenced by the lift force and lift coefficient is calculated using Dynamic Pressure = Lift Force/Lift Coefficient. To calculate Dynamic Pressure given Lift Coefficient, you need Lift Force (FL) & Lift Coefficient (CL). With our tool, you need to enter the respective value for Lift Force & Lift 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 Lift Force & Lift Coefficient. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Dynamic Pressure = Drag Force/Drag 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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