Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) Calculator

✖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.ⓘ Drag Coefficient [C_D]			+10% -10%
✖Distance from X-Axis is defined as the distance from the point where stress is to be computed to XX axis.ⓘ Distance from X-Axis [y]			+10% -10%
✖Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.ⓘ Diameter [d]			+10% -10%

✖Radial Coordinate for an object refers to the coordinate of the object that moves in radial direction from a point of origin.ⓘ Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) [r_cylinder]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Hypersonic Flow Formula PDF PDF Image

Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) Solution

STEP 0: Pre-Calculation Summary

Formula Used

Radial Coordinate = 0.774*Drag Coefficient^(1/3)*(Distance from X-Axis/Diameter)^(2/3)
r_cylinder = 0.774*C_D^(1/3)*(y/d)^(2/3)
This formula uses 4 Variables

Variables Used

Radial Coordinate - (Measured in Meter) - Radial Coordinate for an object refers to the coordinate of the object that moves in radial direction from a point of origin.
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

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

r_cylinder = 0.774*C_D^(1/3)*(y/d)^(2/3) --> 0.774*3.4^(1/3)*(2.2/1.223)^(2/3)

Evaluating ... ...

r_cylinder = 1.72146454399193

STEP 3: Convert Result to Output's Unit

1.72146454399193 Meter -->1721.46454399193 Millimeter (Check conversion here)

FINAL ANSWER

1721.46454399193 ≈ 1721.465 Millimeter <-- Radial Coordinate

(Calculation completed in 00.004 seconds)

You are here -

Home » Engineering » Mechanical » Fluid Mechanics » Hypersonic Flow » Hypersonic Flight Paths Velocity of Altitude Map » Blunt-Nosed Radial Coordinate Flat Plate (First Approximation)

Credits

Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has created this Calculator and 300+ more calculators!

Verified by Shikha Maurya

Indian Institute of Technology (IIT), Bombay

Shikha Maurya has verified this Calculator and 200+ more calculators!

< Hypersonic Flight Paths Velocity of Altitude Map Calculators

Forces Acting Perpendicular to Body on Flight Path

LaTeX Go Lift Force = Weight*cos(Angle of Inclination)-Mass*(Velocity^2)/Radius

Forces Acting on Body along Flight Path

LaTeX Go Drag force along flight path = Weight*sin(Angle of Inclination)-Mass*Velocity Gradient

Radius for Cylinder-Wedge Body Shape

LaTeX Go Radius = Radius of Curvature/(1.386*exp(1.8/(Mach Number-1)^0.75))

Radius for Sphere-Cone Body Shape

LaTeX Go Radius = Radius of Curvature/(1.143*exp(0.54/(Mach Number-1)^1.2))

Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) Formula

LaTeX Go

Radial Coordinate = 0.774*Drag Coefficient^(1/3)*(Distance from X-Axis/Diameter)^(2/3)
r_cylinder = 0.774*C_D^(1/3)*(y/d)^(2/3)

What is blast wave?

In fluid dynamics, a blast wave is the increased pressure and flow resulting from the deposition of a large amount of energy in a small, very localised volume.

How to Calculate Blunt-Nosed Radial Coordinate Flat Plate (First Approximation)?

Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) calculator uses Radial Coordinate = 0.774*Drag Coefficient^(1/3)*(Distance from X-Axis/Diameter)^(2/3) to calculate the Radial Coordinate, Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) formula is defined as a method to estimate the radial distance from the axis of symmetry to the stagnation point on a blunt-nosed body in hypersonic flight, providing a crucial parameter for velocity and altitude mapping in hypersonic flight paths. Radial Coordinate is denoted by r_cylinder symbol.

How to calculate Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) using this online calculator? To use this online calculator for Blunt-Nosed Radial Coordinate Flat Plate (First Approximation), enter Drag Coefficient (C_D), Distance from X-Axis (y) & Diameter (d) and hit the calculate button. Here is how the Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) calculation can be explained with given input values -> 1.7E+6 = 0.774*3.4^(1/3)*(2.2/1.223)^(2/3).

FAQ

What is Blunt-Nosed Radial Coordinate Flat Plate (First Approximation)?

Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) formula is defined as a method to estimate the radial distance from the axis of symmetry to the stagnation point on a blunt-nosed body in hypersonic flight, providing a crucial parameter for velocity and altitude mapping in hypersonic flight paths and is represented as r_cylinder = 0.774*C_D^(1/3)*(y/d)^(2/3) or Radial Coordinate = 0.774*Drag Coefficient^(1/3)*(Distance from X-Axis/Diameter)^(2/3). 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 Blunt-Nosed Radial Coordinate Flat Plate (First Approximation)?

Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) formula is defined as a method to estimate the radial distance from the axis of symmetry to the stagnation point on a blunt-nosed body in hypersonic flight, providing a crucial parameter for velocity and altitude mapping in hypersonic flight paths is calculated using Radial Coordinate = 0.774*Drag Coefficient^(1/3)*(Distance from X-Axis/Diameter)^(2/3). To calculate Blunt-Nosed Radial Coordinate Flat Plate (First Approximation), you need Drag Coefficient (C_D), Distance from X-Axis (y) & Diameter (d). With our tool, you need to enter the respective value for 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.

How many ways are there to calculate Radial Coordinate?

In this formula, Radial Coordinate uses Drag Coefficient, Distance from X-Axis & Diameter. We can use 1 other way(s) to calculate the same, which is/are as follows -

Radial Coordinate = 0.795*Diameter*Drag Coefficient^(1/4)*(Distance from X-Axis/Diameter)^(1/2)

Home

FREE PDFs

🔍 Search