Transformed Conical Variable with Wave Angle Solution

STEP 0: Pre-Calculation Summary
Formula Used
Transformed Conical Variable With Wave Angle = (Wave Angle*(180/pi))/Slenderness Ratio
θwave = (β*(180/pi))/λ
This formula uses 1 Constants, 3 Variables
Constants Used
pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288
Variables Used
Transformed Conical Variable With Wave Angle - Transformed Conical Variable With Wave Angle is the ratio of base radius of cone to product of the slenderness ratio and height of cone at which the radius is taken using wave angle.
Wave Angle - (Measured in Radian) - Wave Angle is the shock angle created by the oblique shock, this is not similar to the mach angle.
Slenderness Ratio - The Slenderness ratio is the ratio of the length of a column and the least radius of gyration of its cross section.
STEP 1: Convert Input(s) to Base Unit
Wave Angle: 0.286 Radian --> 0.286 Radian No Conversion Required
Slenderness Ratio: 0.5 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
θwave = (β*(180/pi))/λ --> (0.286*(180/pi))/0.5
Evaluating ... ...
θwave = 32.7731858814831
STEP 3: Convert Result to Output's Unit
32.7731858814831 --> No Conversion Required
FINAL ANSWER
32.7731858814831 32.77319 <-- Transformed Conical Variable With Wave Angle
(Calculation completed in 00.020 seconds)

Credits

Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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National Institute Of Technology (NIT), Hamirpur
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11 Approximate Methods of Hypersonic Inviscid Flowfields Calculators

Non-Dimensional Pressure for High Mach Number
Go Non Dimensionalized Pressure For High Mech Number = (2*(sin(Wave Angle)^2))/(Specific Heat Ratio+1)
Non-Dimensional Parallel Velocity Component for High Mach Number
Go Non Dimensionalized Upstream Parallel Velocity = 1-(2*(sin(Wave Angle))^2)/(Specific Heat Ratio-1)
Transformed Conical Variable with Wave Angle
Go Transformed Conical Variable With Wave Angle = (Wave Angle*(180/pi))/Slenderness Ratio
Transformed Conical Variable
Go Transformed Conical Variable = Radius of Cone/(Slenderness Ratio*Height of Cone)
Non-Dimensional Radius for Hypersonic Vehicles
Go Non Dimensionalized Radius = Radius of Cone/(Slenderness Ratio*Height of Cone)
Non-Dimensional Perpendicular Velocity Component for High Mach Number
Go Non Dimensionalized Velocity = (sin(2*Wave Angle))/(Specific Heat Ratio-1)
Transformed Conical Variable with Cone Angle in Hypersonic Flow
Go Transformed Conical Variable = (Wave Angle*(180/pi))/Semi Angle of Cone
Non-Dimensional Pressure
Go Non Dimensionalized Pressure = Pressure/(Density*Freestream Velocity^2)
Non-Dimensional Density for High Mach Number
Go Non Dimensionalized Density = (Specific Heat Ratio+1)/(Specific Heat Ratio-1)
Slenderness Ratio with Cone Radius for Hypersonic Vehicle
Go Slenderness Ratio For Hypersonic Vehicles = Radius of Cone/Height of Cone
Non-Dimensional Density
Go Non Dimensionalized Density = Density/Liquid Density

Transformed Conical Variable with Wave Angle Formula

Transformed Conical Variable With Wave Angle = (Wave Angle*(180/pi))/Slenderness Ratio
θwave = (β*(180/pi))/λ

What is a slenderness ratio?

Since the configuration under consideration is slender, the slope at any point is of the
order of ratio of length to diameter of the body

How to Calculate Transformed Conical Variable with Wave Angle?

Transformed Conical Variable with Wave Angle calculator uses Transformed Conical Variable With Wave Angle = (Wave Angle*(180/pi))/Slenderness Ratio to calculate the Transformed Conical Variable With Wave Angle, The Transformed conical variable with wave angle formula is defined as the ratio of wave angle to slenderness ratio. Transformed Conical Variable With Wave Angle is denoted by θwave symbol.

How to calculate Transformed Conical Variable with Wave Angle using this online calculator? To use this online calculator for Transformed Conical Variable with Wave Angle, enter Wave Angle (β) & Slenderness Ratio (λ) and hit the calculate button. Here is how the Transformed Conical Variable with Wave Angle calculation can be explained with given input values -> 32.77319 = (0.286*(180/pi))/0.5.

FAQ

What is Transformed Conical Variable with Wave Angle?
The Transformed conical variable with wave angle formula is defined as the ratio of wave angle to slenderness ratio and is represented as θwave = (β*(180/pi))/λ or Transformed Conical Variable With Wave Angle = (Wave Angle*(180/pi))/Slenderness Ratio. Wave Angle is the shock angle created by the oblique shock, this is not similar to the mach angle & The Slenderness ratio is the ratio of the length of a column and the least radius of gyration of its cross section.
How to calculate Transformed Conical Variable with Wave Angle?
The Transformed conical variable with wave angle formula is defined as the ratio of wave angle to slenderness ratio is calculated using Transformed Conical Variable With Wave Angle = (Wave Angle*(180/pi))/Slenderness Ratio. To calculate Transformed Conical Variable with Wave Angle, you need Wave Angle (β) & Slenderness Ratio (λ). With our tool, you need to enter the respective value for Wave Angle & Slenderness Ratio 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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