Projected Area of Vessel above Waterline given Drag Force due to Wind Solution

STEP 0: Pre-Calculation Summary
Formula Used
Projected Area of the Vessel = Drag Force/(0.5*Air Density*Drag Coefficient*Wind Speed at Height of 10 m^2)
A = FD/(0.5*ρair*CD*V10^2)
This formula uses 5 Variables
Variables Used
Projected Area of the Vessel - (Measured in Square Meter) - Projected Area of the Vessel above the Waterline.
Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid.
Air Density - (Measured in Kilogram per Cubic Meter) - Air Density is the density of wind or air in the atmosphere.
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.
Wind Speed at Height of 10 m - (Measured in Meter per Second) - Wind Speed at Height of 10 m is the ten-meter wind speed measured ten meters above the top of the datum of consideration.
STEP 1: Convert Input(s) to Base Unit
Drag Force: 80 Newton --> 80 Newton No Conversion Required
Air Density: 1.225 Kilogram per Cubic Meter --> 1.225 Kilogram per Cubic Meter No Conversion Required
Drag Coefficient: 30 --> No Conversion Required
Wind Speed at Height of 10 m: 22 Meter per Second --> 22 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
A = FD/(0.5*ρair*CD*V10^2) --> 80/(0.5*1.225*30*22^2)
Evaluating ... ...
A = 0.00899533367065835
STEP 3: Convert Result to Output's Unit
0.00899533367065835 Square Meter --> No Conversion Required
FINAL ANSWER
0.00899533367065835 0.008995 Square Meter <-- Projected Area of the Vessel
(Calculation completed in 00.004 seconds)

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Go Density of Water = (pi*Shear Stress at the Water Surface/Velocity at the Surface)^2/(2*Depth of Frictional Influence*Angular Speed of the Earth*sin(Latitude of the line))
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Go Angle of the Current = acos((Reynolds Number(pb)*Kinematic Viscosity)/(Average Current Speed*Waterline Length of a Vessel))
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Go Kinematic Viscosity = (Average Current Speed*Waterline Length of a Vessel*cos(Angle of the Current))/Reynolds Number
Waterline Length of Vessel given Reynolds Number
Go Waterline Length of a Vessel = (Reynolds Number*Kinematic Viscosity)/Average Current Speed*cos(Angle of the Current)
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Go Average Current Speed = (Reynolds Number*Kinematic Viscosity)/Waterline Length of a Vessel*cos(Angle of the Current)
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Go Density of Air = Drag Force/(0.5*Drag Coefficient*Projected Area of the Vessel*Wind Speed at Height of 10 m^2)
Coefficient of Drag for Winds Measured at 10 m given Drag Force due to Wind
Go Drag Coefficient = Drag Force/(0.5*Air Density*Projected Area of the Vessel*Wind Speed at Height of 10 m^2)
Projected Area of Vessel above Waterline given Drag Force due to Wind
Go Projected Area of the Vessel = Drag Force/(0.5*Air Density*Drag Coefficient*Wind Speed at Height of 10 m^2)
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Go Drag Force = 0.5*Air Density*Drag Coefficient*Projected Area of the Vessel*Wind Speed at Height of 10 m^2
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Projected Area of Vessel above Waterline given Drag Force due to Wind Formula

Projected Area of the Vessel = Drag Force/(0.5*Air Density*Drag Coefficient*Wind Speed at Height of 10 m^2)
A = FD/(0.5*ρair*CD*V10^2)

What factors affect drag?

Drag is influenced by other factors including shape, texture, viscosity (which results in viscous drag or skin friction ), compressibility, lift (which causes induced drag ), boundary layer separation, and so on

How to Calculate Projected Area of Vessel above Waterline given Drag Force due to Wind?

Projected Area of Vessel above Waterline given Drag Force due to Wind calculator uses Projected Area of the Vessel = Drag Force/(0.5*Air Density*Drag Coefficient*Wind Speed at Height of 10 m^2) to calculate the Projected Area of the Vessel, The Projected area of vessel above waterline given drag force due to wind is defined as the parameter influencing the wind load the usual drag equation. Projected Area of the Vessel is denoted by A symbol.

How to calculate Projected Area of Vessel above Waterline given Drag Force due to Wind using this online calculator? To use this online calculator for Projected Area of Vessel above Waterline given Drag Force due to Wind, enter Drag Force (FD), Air Density air), Drag Coefficient (CD) & Wind Speed at Height of 10 m (V10) and hit the calculate button. Here is how the Projected Area of Vessel above Waterline given Drag Force due to Wind calculation can be explained with given input values -> 0.008995 = 80/(0.5*1.225*30*22^2).

FAQ

What is Projected Area of Vessel above Waterline given Drag Force due to Wind?
The Projected area of vessel above waterline given drag force due to wind is defined as the parameter influencing the wind load the usual drag equation and is represented as A = FD/(0.5*ρair*CD*V10^2) or Projected Area of the Vessel = Drag Force/(0.5*Air Density*Drag Coefficient*Wind Speed at Height of 10 m^2). Drag Force is the resisting force experienced by an object moving through a fluid, Air Density is the density of wind or air in the atmosphere, 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 & Wind Speed at Height of 10 m is the ten-meter wind speed measured ten meters above the top of the datum of consideration.
How to calculate Projected Area of Vessel above Waterline given Drag Force due to Wind?
The Projected area of vessel above waterline given drag force due to wind is defined as the parameter influencing the wind load the usual drag equation is calculated using Projected Area of the Vessel = Drag Force/(0.5*Air Density*Drag Coefficient*Wind Speed at Height of 10 m^2). To calculate Projected Area of Vessel above Waterline given Drag Force due to Wind, you need Drag Force (FD), Air Density air), Drag Coefficient (CD) & Wind Speed at Height of 10 m (V10). With our tool, you need to enter the respective value for Drag Force, Air Density, Drag Coefficient & Wind Speed at Height of 10 m and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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