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) - The Wave Angle is the angle between the direction of a hypersonic flow and the wave generated by an oblique shock in fluid mechanics.
Specific Heat Ratio - The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to the heat capacity at constant volume, important for understanding fluid behavior in hypersonic flows.
Deflection Angle - (Measured in Radian) - The Deflection Angle is the angle through which a fluid stream is diverted due to the presence of an obstacle, affecting flow direction in hypersonic conditions.
STEP 1: Convert Input(s) to Base Unit
Specific Heat Ratio: 1.6 --> No Conversion Required
Deflection Angle: 0.39 Radian --> 0.39 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*(0.39*180/pi)*pi/180
Evaluating ... ...
β = 0.507
STEP 3: Convert Result to Output's Unit
0.507 Radian --> No Conversion Required
FINAL ANSWER
0.507 Radian <-- Wave Angle
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Verifier Image
Verified by Anshika Arya
National Institute Of Technology (NIT), Hamirpur
Anshika Arya has verified this Calculator and 2500+ more calculators!

Oblique Shock Relation Calculators

Parallel Upstream Flow Components after Shock as Mach Tends to Infinite
​ LaTeX ​ 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
​ LaTeX ​ Go Perpendicular upstream flow components = (Velocity of the fluid at 1*sin(2*Wave Angle))/(Specific Heat Ratio-1)
Wave Angle for Small Deflection Angle
​ LaTeX ​ Go Wave Angle = (Specific Heat Ratio+1)/2*(Deflection Angle*180/pi)*pi/180
Coefficient of Pressure Derived from Oblique Shock Theory
​ LaTeX ​ Go Pressure Coefficient = 2*(sin(Wave Angle))^2

Wave Angle for Small Deflection Angle Formula

​LaTeX ​Go
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 a measure of the angle of a shock wave that occurs when a supersonic flow encounters a sudden change in direction, allowing engineers to analyze and predict the behavior of oblique shock waves in various applications. 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 -> 0.52 = (1.6+1)/2*(0.39*180/pi)*pi/180.

FAQ

What is Wave Angle for Small Deflection Angle?
Wave Angle for Small Deflection Angle formula is defined as a measure of the angle of a shock wave that occurs when a supersonic flow encounters a sudden change in direction, allowing engineers to analyze and predict the behavior of oblique shock waves in various applications 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 is the ratio of the heat capacity at constant pressure to the heat capacity at constant volume, important for understanding fluid behavior in hypersonic flows & The Deflection Angle is the angle through which a fluid stream is diverted due to the presence of an obstacle, affecting flow direction in hypersonic conditions.
How to calculate Wave Angle for Small Deflection Angle?
Wave Angle for Small Deflection Angle formula is defined as a measure of the angle of a shock wave that occurs when a supersonic flow encounters a sudden change in direction, allowing engineers to analyze and predict the behavior of oblique shock waves in various applications 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.
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!