Dynamic pressure aircraft Calculator

✖Ambient Air Density is the mass per unit volume of Earth's atmosphere.ⓘ Ambient Air Density [ρ]			+10% -10%
✖Flight Speed is defined as an airspeed sufficient to provide the lift necessary to support an airplane in level flight.ⓘ Flight Speed [V_fs]			+10% -10%

✖Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.ⓘ Dynamic pressure aircraft [q]

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Dynamic pressure aircraft Solution

STEP 0: Pre-Calculation Summary

Formula Used

Dynamic Pressure = 1/2*Ambient Air Density*Flight Speed^2
q = 1/2*ρ*V_fs^2
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.
Ambient Air Density - (Measured in Kilogram per Cubic Meter) - Ambient Air Density is the mass per unit volume of Earth's atmosphere.
Flight Speed - (Measured in Meter per Second) - Flight Speed is defined as an airspeed sufficient to provide the lift necessary to support an airplane in level flight.

STEP 1: Convert Input(s) to Base Unit

Ambient Air Density: 1.225 Kilogram per Cubic Meter --> 1.225 Kilogram per Cubic Meter No Conversion Required
Flight Speed: 10.73 Meter per Second --> 10.73 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

q = 1/2*ρ*V_fs^2 --> 1/2*1.225*10.73^2

Evaluating ... ...

q = 70.51890125

STEP 3: Convert Result to Output's Unit

70.51890125 Pascal --> No Conversion Required

FINAL ANSWER

70.51890125 ≈ 70.5189 Pascal <-- Dynamic Pressure

(Calculation completed in 00.004 seconds)

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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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< 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 aircraft Formula

LaTeX Go

Dynamic Pressure = 1/2*Ambient Air Density*Flight Speed^2
q = 1/2*ρ*V_fs^2

What is dynamic pressure?

Dynamic 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 aircraft?

Dynamic pressure aircraft calculator uses Dynamic Pressure = 1/2*Ambient Air Density*Flight Speed^2 to calculate the Dynamic Pressure, Dynamic Pressure Aircraft is a measure of the pressure exerted on an object as it moves through the air, calculated by considering the density of the ambient air and the speed of the aircraft, providing a crucial parameter in aerodynamics to estimate the forces acting on an aircraft in flight. Dynamic Pressure is denoted by q symbol.

How to calculate Dynamic pressure aircraft using this online calculator? To use this online calculator for Dynamic pressure aircraft, enter Ambient Air Density (ρ) & Flight Speed (V_fs) and hit the calculate button. Here is how the Dynamic pressure aircraft calculation can be explained with given input values -> 27528.2 = 1/2*1.225*10.73^2.

FAQ

What is Dynamic pressure aircraft?

Dynamic Pressure Aircraft is a measure of the pressure exerted on an object as it moves through the air, calculated by considering the density of the ambient air and the speed of the aircraft, providing a crucial parameter in aerodynamics to estimate the forces acting on an aircraft in flight and is represented as q = 1/2*ρ*V_fs^2 or Dynamic Pressure = 1/2*Ambient Air Density*Flight Speed^2. Ambient Air Density is the mass per unit volume of Earth's atmosphere & Flight Speed is defined as an airspeed sufficient to provide the lift necessary to support an airplane in level flight.

How to calculate Dynamic pressure aircraft?

Dynamic Pressure Aircraft is a measure of the pressure exerted on an object as it moves through the air, calculated by considering the density of the ambient air and the speed of the aircraft, providing a crucial parameter in aerodynamics to estimate the forces acting on an aircraft in flight is calculated using Dynamic Pressure = 1/2*Ambient Air Density*Flight Speed^2. To calculate Dynamic pressure aircraft, you need Ambient Air Density (ρ) & Flight Speed (V_fs). With our tool, you need to enter the respective value for Ambient Air Density & Flight Speed 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 Ambient Air Density & Flight Speed. We can use 3 other way(s) to calculate the same, which is/are as follows -

Dynamic Pressure = Lift Force/Lift Coefficient
Dynamic Pressure = Drag Force/Drag Coefficient
Dynamic Pressure = 1/2*Ambient Air Density*(Mach Number*Sonic Speed)^2

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