Pressure Ratio of Blunt-Nosed Cylinder (First Approximation) Solution

STEP 0: Pre-Calculation Summary
Formula Used
Pressure Ratio = 0.067*Mach Number Cylinder^2*sqrt(Drag Coefficient)/(Distance from X-Axis/Diameter)
rp = 0.067*Mcylinder^2*sqrt(CD)/(y/d)
This formula uses 1 Functions, 5 Variables
Functions Used
sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)
Variables Used
Pressure Ratio - Pressure Ratio is ratio of final to initial pressure.
Mach Number Cylinder - Mach number Cylinder is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
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.
Distance from X-Axis - (Measured in Meter) - Distance from X-Axis is defined as the distance from the point where stress is to be computed to XX axis.
Diameter - (Measured in Meter) - Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.
STEP 1: Convert Input(s) to Base Unit
Mach Number Cylinder: 3.7 --> No Conversion Required
Drag Coefficient: 3.4 --> No Conversion Required
Distance from X-Axis: 2200 Millimeter --> 2.2 Meter (Check conversion ​here)
Diameter: 1223 Millimeter --> 1.223 Meter (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
rp = 0.067*Mcylinder^2*sqrt(CD)/(y/d) --> 0.067*3.7^2*sqrt(3.4)/(2.2/1.223)
Evaluating ... ...
rp = 0.940202681692205
STEP 3: Convert Result to Output's Unit
0.940202681692205 --> No Conversion Required
FINAL ANSWER
0.940202681692205 0.940203 <-- Pressure Ratio
(Calculation completed in 00.004 seconds)

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Pressure Ratio of Blunt-Nosed Cylinder (First Approximation) Formula

​LaTeX ​Go
Pressure Ratio = 0.067*Mach Number Cylinder^2*sqrt(Drag Coefficient)/(Distance from X-Axis/Diameter)
rp = 0.067*Mcylinder^2*sqrt(CD)/(y/d)

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How to Calculate Pressure Ratio of Blunt-Nosed Cylinder (First Approximation)?

Pressure Ratio of Blunt-Nosed Cylinder (First Approximation) calculator uses Pressure Ratio = 0.067*Mach Number Cylinder^2*sqrt(Drag Coefficient)/(Distance from X-Axis/Diameter) to calculate the Pressure Ratio, Pressure ratio of Blunt-nosed cylinder (first approximation) formula is defined as interrelation between drag coefficient, mach number at infinity, distance from the tip of the slab and base diameter. Pressure Ratio is denoted by rp symbol.

How to calculate Pressure Ratio of Blunt-Nosed Cylinder (First Approximation) using this online calculator? To use this online calculator for Pressure Ratio of Blunt-Nosed Cylinder (First Approximation), enter Mach Number Cylinder (Mcylinder), Drag Coefficient (CD), Distance from X-Axis (y) & Diameter (d) and hit the calculate button. Here is how the Pressure Ratio of Blunt-Nosed Cylinder (First Approximation) calculation can be explained with given input values -> 0.940203 = 0.067*3.7^2*sqrt(3.4)/(2.2/1.223).

FAQ

What is Pressure Ratio of Blunt-Nosed Cylinder (First Approximation)?
Pressure ratio of Blunt-nosed cylinder (first approximation) formula is defined as interrelation between drag coefficient, mach number at infinity, distance from the tip of the slab and base diameter and is represented as rp = 0.067*Mcylinder^2*sqrt(CD)/(y/d) or Pressure Ratio = 0.067*Mach Number Cylinder^2*sqrt(Drag Coefficient)/(Distance from X-Axis/Diameter). Mach number Cylinder is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound, 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, Distance from X-Axis is defined as the distance from the point where stress is to be computed to XX axis & Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.
How to calculate Pressure Ratio of Blunt-Nosed Cylinder (First Approximation)?
Pressure ratio of Blunt-nosed cylinder (first approximation) formula is defined as interrelation between drag coefficient, mach number at infinity, distance from the tip of the slab and base diameter is calculated using Pressure Ratio = 0.067*Mach Number Cylinder^2*sqrt(Drag Coefficient)/(Distance from X-Axis/Diameter). To calculate Pressure Ratio of Blunt-Nosed Cylinder (First Approximation), you need Mach Number Cylinder (Mcylinder), Drag Coefficient (CD), Distance from X-Axis (y) & Diameter (d). With our tool, you need to enter the respective value for Mach Number Cylinder, Drag Coefficient, Distance from X-Axis & Diameter 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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