Dynamic Pressure given Coefficient of Lift Solution

STEP 0: Pre-Calculation Summary
Formula Used
Dynamic Pressure = Lift Force/(Lift Coefficient*Area For Flow)
q = FL/(CL*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.
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.
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
Lift Force: 10.5 Newton --> 10.5 Newton No Conversion Required
Lift Coefficient: 0.021 --> 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 = FL/(CL*A) --> 10.5/(0.021*50)
Evaluating ... ...
q = 10
STEP 3: Convert Result to Output's Unit
10 Pascal --> No Conversion Required
FINAL ANSWER
10 Pascal <-- Dynamic Pressure
(Calculation completed in 00.006 seconds)

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Amrita School of Engineering (ASE), Vallikavu
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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 given Coefficient of Lift Formula

​LaTeX ​Go
Dynamic Pressure = Lift Force/(Lift Coefficient*Area For Flow)
q = FL/(CL*A)

What is dynamic pressure?

In fluid dynamics, drag (sometimes called air resistance, a type of friction, or fluid resistance, another type of friction or fluid friction) is a force acting opposite to the relative motion of any object moving with respect to a surrounding fluid.[1] This can exist between two fluid layers (or surfaces) or a fluid and a solid surface

How to Calculate Dynamic Pressure given Coefficient of Lift?

Dynamic Pressure given Coefficient of Lift calculator uses Dynamic Pressure = Lift Force/(Lift Coefficient*Area For Flow) to calculate the Dynamic Pressure, Dynamic Pressure given Coefficient of Lift formula is defined as a measure of the pressure exerted on an object as it moves through a fluid, typically air, at high velocities, and is a critical parameter in the study of hypersonic flow and aerodynamics. Dynamic Pressure is denoted by q symbol.

How to calculate Dynamic Pressure given Coefficient of Lift using this online calculator? To use this online calculator for Dynamic Pressure given Coefficient of Lift, enter Lift Force (FL), Lift Coefficient (CL) & Area For Flow (A) and hit the calculate button. Here is how the Dynamic Pressure given Coefficient of Lift calculation can be explained with given input values -> 0.190909 = 10.5/(0.021*50).

FAQ

What is Dynamic Pressure given Coefficient of Lift?
Dynamic Pressure given Coefficient of Lift formula is defined as a measure of the pressure exerted on an object as it moves through a fluid, typically air, at high velocities, and is a critical parameter in the study of hypersonic flow and aerodynamics and is represented as q = FL/(CL*A) or Dynamic Pressure = Lift Force/(Lift Coefficient*Area For Flow). 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 & 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 given Coefficient of Lift?
Dynamic Pressure given Coefficient of Lift formula is defined as a measure of the pressure exerted on an object as it moves through a fluid, typically air, at high velocities, and is a critical parameter in the study of hypersonic flow and aerodynamics is calculated using Dynamic Pressure = Lift Force/(Lift Coefficient*Area For Flow). To calculate Dynamic Pressure given Coefficient of Lift, you need Lift Force (FL), Lift Coefficient (CL) & Area For Flow (A). With our tool, you need to enter the respective value for Lift Force, Lift 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 Lift Force, Lift Coefficient & Area For Flow. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Dynamic Pressure = Drag Force/(Drag Coefficient*Area For Flow)
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