Wave Angle for Small Deflection Angle Solution

STEP 0: Pre-Calculation Summary
Formula Used
Wave Angle = (Specific Heat Ratio+1)/2*(Deflection Angle*180/pi)*pi/180
β = (Y+1)/2*(θd*180/pi)*pi/180
This formula uses 1 Constants, 3 Variables
Constants Used
pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288
Variables Used
Wave Angle - (Measured in Radian) - Wave Angle is the shock angle created by the oblique shock, this is not similar to the mach angle.
Specific Heat Ratio - The Specific heat ratio of a gas is the ratio of the specific heat of the gas at a constant pressure to its specific heat at a constant volume.
Deflection Angle - (Measured in Radian) - A Deflection angle is the angle between the onward extension of the previous leg and the line ahead.
STEP 1: Convert Input(s) to Base Unit
Specific Heat Ratio: 1.6 --> No Conversion Required
Deflection Angle: 0.191986 Radian --> 0.191986 Radian No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
β = (Y+1)/2*(θd*180/pi)*pi/180 --> (1.6+1)/2*(0.191986*180/pi)*pi/180
Evaluating ... ...
β = 0.2495818
STEP 3: Convert Result to Output's Unit
0.2495818 Radian --> No Conversion Required
FINAL ANSWER
0.2495818 0.249582 Radian <-- Wave Angle
(Calculation completed in 00.004 seconds)

Credits

Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Verified by Anshika Arya
National Institute Of Technology (NIT), Hamirpur
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15 Oblique Shock Relation Calculators

Exact Density Ratio
Go Density Ratio = ((Specific Heat Ratio+1)*(Mach Number*(sin(Wave Angle)))^2)/((Specific Heat Ratio-1)*(Mach Number*(sin(Wave Angle)))^2+2)
Temperature Ratio when Mach Becomes Infinite
Go Temperature Ratio = (2*Specific Heat Ratio*(Specific Heat Ratio-1))/(Specific Heat Ratio+1)^2*(Mach Number*sin(Wave Angle))^2
Exact Pressure Ratio
Go Pressure Ratio = 1+2*Specific Heat Ratio/(Specific Heat Ratio+1)*((Mach Number*sin(Wave Angle))^2-1)
Pressure Ratio when Mach becomes Infinite
Go Pressure Ratio = (2*Specific Heat Ratio)/(Specific Heat Ratio+1)*(Mach Number*sin(Wave Angle))^2
Parallel Upstream Flow Components after Shock as Mach Tends to Infinite
Go Parallel upstream flow components = Velocity of the fluid at 1*(1-(2*(sin(Wave Angle))^2)/(Specific Heat Ratio-1))
Perpendicular Upstream Flow Components behind Shock Wave
Go Perpendicular upstream flow components = (Velocity of the fluid at 1*(sin(2*Wave Angle)))/(Specific Heat Ratio-1)
Pressure Coefficient behind Oblique Shock Wave
Go Pressure Coefficient = 4/(Specific Heat Ratio+1)*((sin(Wave Angle))^2-1/Mach Number^2)
Wave Angle for Small Deflection Angle
Go Wave Angle = (Specific Heat Ratio+1)/2*(Deflection Angle*180/pi)*pi/180
Velocity of Sound using Dynamic Pressure and Density
Go Speed of Sound = sqrt((Specific Heat Ratio*Pressure)/Density)
Dynamic Pressure for given Specific Heat Ratio and Mach Number
Go Dynamic Pressure = Specific Heat Ratio Dynamic*Static Pressure*(Mach Number^2)/2
Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number
Go Pressure Coefficient = 4/(Specific Heat Ratio+1)*(sin(Wave Angle))^2
Non-Dimensional Pressure Coefficient
Go Pressure Coefficient = Change in static pressure/Dynamic Pressure
Density Ratio when Mach Becomes Infinite
Go Density Ratio = (Specific Heat Ratio+1)/(Specific Heat Ratio-1)
Temperature Ratios
Go Temperature Ratio = Pressure Ratio/Density Ratio
Coefficient of Pressure Derived from Oblique Shock Theory
Go Pressure Coefficient = 2*(sin(Wave Angle))^2

Wave Angle for Small Deflection Angle Formula

Wave Angle = (Specific Heat Ratio+1)/2*(Deflection Angle*180/pi)*pi/180
β = (Y+1)/2*(θd*180/pi)*pi/180

what are the changes due to small deflection angle?

When the deflection angle is small the value of wave angle becomes 1.2 times the deflection angle. It is interesting to observe that, in the hypersonic limit for a slender wedge, the
wave angle is only 20% larger than the wedge angle—

How to Calculate Wave Angle for Small Deflection Angle?

Wave Angle for Small Deflection Angle calculator uses Wave Angle = (Specific Heat Ratio+1)/2*(Deflection Angle*180/pi)*pi/180 to calculate the Wave Angle, Wave angle for small deflection angle formula is defined as the product of specific heat ratio and deflection angle. Wave Angle is denoted by β symbol.

How to calculate Wave Angle for Small Deflection Angle using this online calculator? To use this online calculator for Wave Angle for Small Deflection Angle, enter Specific Heat Ratio (Y) & Deflection Angle d) and hit the calculate button. Here is how the Wave Angle for Small Deflection Angle calculation can be explained with given input values -> 0.249582 = (1.6+1)/2*(0.191986*180/pi)*pi/180.

FAQ

What is Wave Angle for Small Deflection Angle?
Wave angle for small deflection angle formula is defined as the product of specific heat ratio and deflection angle and is represented as β = (Y+1)/2*(θd*180/pi)*pi/180 or Wave Angle = (Specific Heat Ratio+1)/2*(Deflection Angle*180/pi)*pi/180. The Specific heat ratio of a gas is the ratio of the specific heat of the gas at a constant pressure to its specific heat at a constant volume & A Deflection angle is the angle between the onward extension of the previous leg and the line ahead.
How to calculate Wave Angle for Small Deflection Angle?
Wave angle for small deflection angle formula is defined as the product of specific heat ratio and deflection angle is calculated using Wave Angle = (Specific Heat Ratio+1)/2*(Deflection Angle*180/pi)*pi/180. To calculate Wave Angle for Small Deflection Angle, you need Specific Heat Ratio (Y) & Deflection Angle d). With our tool, you need to enter the respective value for Specific Heat Ratio & Deflection Angle 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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