Nose Radius of Cylinder-Wedge Formula

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Radius is a radial line from the focus to any point of a curve. Check FAQs
r=𝛿0.386exp(4.67M2)
r - Radius?𝛿 - Local Shock-Detachment Distance?M - Mach Number?

Nose Radius of Cylinder-Wedge Example

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With units
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Here is how the Nose Radius of Cylinder-Wedge equation looks like with Values.

Here is how the Nose Radius of Cylinder-Wedge equation looks like with Units.

Here is how the Nose Radius of Cylinder-Wedge equation looks like.

57.1987Edit=23.75Edit0.386exp(4.678Edit2)
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Nose Radius of Cylinder-Wedge Solution

Follow our step by step solution on how to calculate Nose Radius of Cylinder-Wedge?

FIRST Step Consider the formula
r=𝛿0.386exp(4.67M2)
Next Step Substitute values of Variables
r=23.75mm0.386exp(4.6782)
Next Step Convert Units
r=0.0238m0.386exp(4.6782)
Next Step Prepare to Evaluate
r=0.02380.386exp(4.6782)
Next Step Evaluate
r=0.0571987296943239m
Next Step Convert to Output's Unit
r=57.1987296943239mm
LAST Step Rounding Answer
r=57.1987mm

Nose Radius of Cylinder-Wedge Formula Elements

Variables
Functions
Radius
Radius is a radial line from the focus to any point of a curve.
Symbol: r
Measurement: LengthUnit: mm
Note: Value should be greater than 0.
Local Shock-Detachment Distance
Local shock-Detachment Distance is the distance of shock formation from leading edge.
Symbol: 𝛿
Measurement: LengthUnit: mm
Note: Value should be greater than 0.
Mach Number
Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
Symbol: M
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
exp
n an exponential function, the value of the function changes by a constant factor for every unit change in the independent variable.
Syntax: exp(Number)

Other formulas in Shock Dynamics and Aerodynamic Shape category

​Go Grid Point Calculation for Shock Waves
ζ=y-b𝛿
​Go Mach Wave behind Shock
M2=V-Wmcs
​Go Mach Wave behind Shock with Mach Infinity
M1=M-Wcs
​Go Local Shock Velocity Equation
W=cs(M-M1)

How to Evaluate Nose Radius of Cylinder-Wedge?

Nose Radius of Cylinder-Wedge evaluator uses Radius = Local Shock-Detachment Distance/(0.386*exp(4.67/(Mach Number^2))) to evaluate the Radius, The Nose Radius of Cylinder-Wedge formula is defined as a measure of the radius of a cylinder-wedge shape in hypersonic inviscid flow, which is critical in understanding the aerodynamic characteristics of vehicles and projectiles at high speeds, particularly in the context of re-entry vehicles and spacecraft. Radius is denoted by r symbol.

How to evaluate Nose Radius of Cylinder-Wedge using this online evaluator? To use this online evaluator for Nose Radius of Cylinder-Wedge, enter Local Shock-Detachment Distance (𝛿) & Mach Number (M) and hit the calculate button.

FAQs on Nose Radius of Cylinder-Wedge

What is the formula to find Nose Radius of Cylinder-Wedge?
The formula of Nose Radius of Cylinder-Wedge is expressed as Radius = Local Shock-Detachment Distance/(0.386*exp(4.67/(Mach Number^2))). Here is an example- 46481.49 = 0.02375/(0.386*exp(4.67/(8^2))).
How to calculate Nose Radius of Cylinder-Wedge?
With Local Shock-Detachment Distance (𝛿) & Mach Number (M) we can find Nose Radius of Cylinder-Wedge using the formula - Radius = Local Shock-Detachment Distance/(0.386*exp(4.67/(Mach Number^2))). This formula also uses Exponential Growth (exp) function(s).
Can the Nose Radius of Cylinder-Wedge be negative?
No, the Nose Radius of Cylinder-Wedge, measured in Length cannot be negative.
Which unit is used to measure Nose Radius of Cylinder-Wedge?
Nose Radius of Cylinder-Wedge is usually measured using the Millimeter[mm] for Length. Meter[mm], Kilometer[mm], Decimeter[mm] are the few other units in which Nose Radius of Cylinder-Wedge can be measured.
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