Doty and Rasmussen- Normal Force Coefficient Formula

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Coefficient of Force is the force acting on the reference area with dynamic pressure in the case of hypersonic flow. Check FAQs
μ=2FnρfluidU2A
μ - Coefficient of Force?Fn - Normal Force?ρfluid - Density of Fluid?U - Freestream Velocity Normal?A - Area?

Doty and Rasmussen- Normal Force Coefficient Example

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Here is how the Doty and Rasmussen- Normal Force Coefficient equation looks like with Values.

Here is how the Doty and Rasmussen- Normal Force Coefficient equation looks like with Units.

Here is how the Doty and Rasmussen- Normal Force Coefficient equation looks like.

0.4171Edit=257.3Edit13.9Edit102Edit20.0019Edit
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Doty and Rasmussen- Normal Force Coefficient Solution

Follow our step by step solution on how to calculate Doty and Rasmussen- Normal Force Coefficient?

FIRST Step Consider the formula
μ=2FnρfluidU2A
Next Step Substitute values of Variables
μ=257.3N13.9kg/m³102m/s20.0019
Next Step Prepare to Evaluate
μ=257.313.910220.0019
Next Step Evaluate
μ=0.417076646459194
LAST Step Rounding Answer
μ=0.4171

Doty and Rasmussen- Normal Force Coefficient Formula Elements

Variables
Coefficient of Force
Coefficient of Force is the force acting on the reference area with dynamic pressure in the case of hypersonic flow.
Symbol: μ
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Normal Force
Normal Force is the force which is normal to the shear force.
Symbol: Fn
Measurement: ForceUnit: N
Note: Value can be positive or negative.
Density of Fluid
Density of Fluid is defined as the mass of fluid per unit volume of the said fluid.
Symbol: ρfluid
Measurement: DensityUnit: kg/m³
Note: Value should be greater than 0.
Freestream Velocity Normal
Freestream Velocity Normal is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air.
Symbol: U
Measurement: SpeedUnit: m/s
Note: Value can be positive or negative.
Area
The Area is the amount of two-dimensional space taken up by an object.
Symbol: A
Measurement: AreaUnit:
Note: Value should be greater than 0.

Other formulas in Hypersonic Flow and Disturbances category

​Go Change in Velocity for Hypersonic Flow in X Direction
u'=vfluid-U
​Go Similarity Constant Equation with Slenderness Ratio
K=Mλ
​Go Density Ratio with Similarity Constant having Slenderness Ratio
ρratio=(γ+1γ-1)(11+2(γ-1)K2)
​Go Coefficient of Pressure with Slenderness Ratio
Cp=2γM2(p-γM2λ2-1)

How to Evaluate Doty and Rasmussen- Normal Force Coefficient?

Doty and Rasmussen- Normal Force Coefficient evaluator uses Coefficient of Force = 2*Normal Force/(Density of Fluid*Freestream Velocity Normal^2*Area) to evaluate the Coefficient of Force, Doty and Rasmussen- Normal Force Coefficient formula is defined as a dimensionless quantity that characterizes the normal force exerted on a body in hypersonic flow, providing a crucial parameter in the study of hypersonic flow and disturbances, where the normal force coefficient is essential in understanding the aerodynamic behavior of vehicles at high speeds. Coefficient of Force is denoted by μ symbol.

How to evaluate Doty and Rasmussen- Normal Force Coefficient using this online evaluator? To use this online evaluator for Doty and Rasmussen- Normal Force Coefficient, enter Normal Force (Fn), Density of Fluid fluid), Freestream Velocity Normal (U) & Area (A) and hit the calculate button.

FAQs on Doty and Rasmussen- Normal Force Coefficient

What is the formula to find Doty and Rasmussen- Normal Force Coefficient?
The formula of Doty and Rasmussen- Normal Force Coefficient is expressed as Coefficient of Force = 2*Normal Force/(Density of Fluid*Freestream Velocity Normal^2*Area). Here is an example- 0.417077 = 2*57.3/(13.9*102^2*0.0019).
How to calculate Doty and Rasmussen- Normal Force Coefficient?
With Normal Force (Fn), Density of Fluid fluid), Freestream Velocity Normal (U) & Area (A) we can find Doty and Rasmussen- Normal Force Coefficient using the formula - Coefficient of Force = 2*Normal Force/(Density of Fluid*Freestream Velocity Normal^2*Area).
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