Dynamic pressure given lift coefficient Solution

STEP 0: Pre-Calculation Summary
Formula Used
Dynamic Pressure = Lift Force/Lift Coefficient
Pdynamic = L/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: 1000 Newton --> 1000 Newton No Conversion Required
Lift Coefficient: 1.1 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Pdynamic = L/CL --> 1000/1.1
Evaluating ... ...
Pdynamic = 909.090909090909
STEP 3: Convert Result to Output's Unit
909.090909090909 Pascal --> No Conversion Required
909.090909090909 Pascal <-- Dynamic Pressure
(Calculation completed in 00.016 seconds)
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Created by Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
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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
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
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
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
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
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
Dynamic Pressure = Drag Force/Drag Coefficient

Dynamic pressure given lift coefficient Formula

Dynamic Pressure = Lift Force/Lift Coefficient
Pdynamic = L/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, The Dynamic pressure given lift coefficient formula is defined as dynamic pressure is equal to 0.5 times the air density times the airspeed squared, so dynamic pressure can be used to determine the airspeed of the aircraft. Dynamic Pressure is denoted by Pdynamic 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 (L) & 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 -> 909.0909 = 1000/1.1.

FAQ

What is Dynamic pressure given lift coefficient?
The Dynamic pressure given lift coefficient formula is defined as dynamic pressure is equal to 0.5 times the air density times the airspeed squared, so dynamic pressure can be used to determine the airspeed of the aircraft and is represented as Pdynamic = L/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?
The Dynamic pressure given lift coefficient formula is defined as dynamic pressure is equal to 0.5 times the air density times the airspeed squared, so dynamic pressure can be used to determine the airspeed of the aircraft is calculated using Dynamic Pressure = Lift Force/Lift Coefficient. To calculate Dynamic pressure given lift coefficient, you need Lift Force (L) & 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 5 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
• 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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