Speed of Sound Solution

STEP 0: Pre-Calculation Summary
Formula Used
Speed of Sound = sqrt(Specific Heat Ratio*[R-Dry-Air]*Static Temperature)
a = sqrt(γ*[R-Dry-Air]*Ts)
This formula uses 1 Constants, 1 Functions, 3 Variables
Constants Used
[R-Dry-Air] - Specific Gas Constant for Dry Air Value Taken As 287.058
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
Speed of Sound - (Measured in Meter per Second) - The Speed of Sound is defined as speed of the dynamic propagation of sound waves.
Specific Heat Ratio - The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume of the flowing fluid for non-viscous and compressible flow.
Static Temperature - (Measured in Kelvin) - The Static Temperature is defined as the temperature measured by a thermometer placed within the fluid without affecting the fluid's velocity or pressure.
STEP 1: Convert Input(s) to Base Unit
Specific Heat Ratio: 1.4 --> No Conversion Required
Static Temperature: 296 Kelvin --> 296 Kelvin No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
a = sqrt(γ*[R-Dry-Air]*Ts) --> sqrt(1.4*[R-Dry-Air]*296)
Evaluating ... ...
a = 344.901196286705
STEP 3: Convert Result to Output's Unit
344.901196286705 Meter per Second --> No Conversion Required
FINAL ANSWER
344.901196286705 344.9012 Meter per Second <-- Speed of Sound
(Calculation completed in 00.004 seconds)

Credits

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Created by Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
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Verified by Rushi Shah
K J Somaiya College of Engineering (K J Somaiya), Mumbai
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19 Thermodynamics and Governing Equations Calculators

Max work output in Brayton cycle
​ Go Maximum Work done in Brayton Cycle = (1005*1/Compressor Efficiency)*Temperature at Inlet of Compressor in Brayton*(sqrt(Temperature at Inlet to Turbine in Brayton Cycle/Temperature at Inlet of Compressor in Brayton*Compressor Efficiency*Turbine Efficiency)-1)^2
Choked Mass Flow Rate given specific heat ratio
​ Go Choked Mass Flow Rate = (Heat Capacity Ratio/(sqrt(Heat Capacity Ratio-1)))*((Heat Capacity Ratio+1)/2)^(-((Heat Capacity Ratio+1)/(2*Heat Capacity Ratio-2)))
Choked Mass Flow Rate
​ Go Choked Mass Flow Rate = (Mass Flow Rate*sqrt(Specific Heat Capacity at Constant Pressure*Temperature))/(Nozzle Throat Area*Throat Pressure)
Stagnation Velocity of Sound given Specific Heat at Constant Pressure
​ Go Stagnation Velocity of Sound = sqrt((Heat Capacity Ratio-1)*Specific Heat Capacity at Constant Pressure*Stagnation Temperature)
Specific Heat of mixed out gas
​ Go Specific Heat of Mixed Gas = (Specific Heat of Core Gas+Bypass Ratio*Specific Heat of Bypass Air)/(1+Bypass Ratio)
Stagnation Temperature
​ Go Stagnation Temperature = Static Temperature+(Flow Velocity Downstream of Sound^2)/(2*Specific Heat Capacity at Constant Pressure)
Stagnation Velocity of Sound
​ Go Stagnation Velocity of Sound = sqrt(Heat Capacity Ratio*[R]*Stagnation Temperature)
Speed of Sound
​ Go Speed of Sound = sqrt(Specific Heat Ratio*[R-Dry-Air]*Static Temperature)
Stagnation Velocity of Sound given Stagnation Enthalpy
​ Go Stagnation Velocity of Sound = sqrt((Heat Capacity Ratio-1)*Stagnation Enthalpy)
Heat Capacity Ratio
​ Go Heat Capacity Ratio = Specific Heat Capacity at Constant Pressure/Specific Heat Capacity at Constant Volume
Efficiency of cycle
​ Go Efficiency of Cycle = (Turbine Work-Compressor Work)/Heat
Internal Energy of Perfect Gas at given Temperature
​ Go Internal Energy = Specific Heat Capacity at Constant Volume*Temperature
Enthalpy of Ideal Gas at given Temperature
​ Go Enthalpy = Specific Heat Capacity at Constant Pressure*Temperature
Stagnation enthalpy
​ Go Stagnation Enthalpy = Enthalpy+(Velocity of Fluid Flow^2)/2
Efficiency of Joule cycle
​ Go Efficiency of Joule Cycle = Net Work Output/Heat
Pressure Ratio
​ Go Pressure Ratio = Final Pressure/Initial Pressure
Work ratio in practical cycle
​ Go Work Ratio = 1-(Compressor Work/Turbine Work)
Mach Number
​ Go Mach Number = Speed of Object/Speed of Sound
Mach Angle
​ Go Mach Angle = asin(1/Mach Number)

18 Governing Equations and Sound Wave Calculators

Speed of Sound Downstream of Sound Wave
​ Go Sound Speed Downstream = sqrt((Specific Heat Ratio-1)*((Flow Velocity Upstream of Sound^2-Flow Velocity Downstream of Sound^2)/2+Sound Speed Upstream^2/(Specific Heat Ratio-1)))
Speed of Sound Upstream of Sound Wave
​ Go Sound Speed Upstream = sqrt((Specific Heat Ratio-1)*((Flow Velocity Downstream of Sound^2-Flow Velocity Upstream of Sound^2)/2+Sound Speed Downstream^2/(Specific Heat Ratio-1)))
Flow Velocity Downstream of Sound Wave
​ Go Flow Velocity Downstream of Sound = sqrt(2*((Sound Speed Upstream^2-Sound Speed Downstream^2)/(Specific Heat Ratio-1)+Flow Velocity Upstream of Sound^2/2))
Flow Velocity Upstream of Sound Wave
​ Go Flow Velocity Upstream of Sound = sqrt(2*((Sound Speed Downstream^2-Sound Speed Upstream^2)/(Specific Heat Ratio-1)+Flow Velocity Downstream of Sound^2/2))
Ratio of Stagnation and Static Pressure
​ Go Stagnation to Static Pressure = (1+((Specific Heat Ratio-1)/2)*Mach Number^2)^(Specific Heat Ratio/(Specific Heat Ratio-1))
Critical Pressure
​ Go Critical Pressure = (2/(Specific Heat Ratio+1))^(Specific Heat Ratio/(Specific Heat Ratio-1))*Stagnation Pressure
Stagnation Temperature
​ Go Stagnation Temperature = Static Temperature+(Flow Velocity Downstream of Sound^2)/(2*Specific Heat Capacity at Constant Pressure)
Speed of Sound
​ Go Speed of Sound = sqrt(Specific Heat Ratio*[R-Dry-Air]*Static Temperature)
Ratio of Stagnation and Static Density
​ Go Stagnation to Static Density = (1+((Specific Heat Ratio-1)/2)*Mach Number^2)^(1/(Specific Heat Ratio-1))
Critical Density
​ Go Critical Density = Stagnation Density*(2/(Specific Heat Ratio+1))^(1/(Specific Heat Ratio-1))
Mayer's Formula
​ Go Specific Gas Constant = Specific Heat Capacity at Constant Pressure-Specific Heat Capacity at Constant Volume
Ratio of Stagnation and Static Temperature
​ Go Stagnation to Static Temperature = 1+((Specific Heat Ratio-1)/2)*Mach Number^2
Critical Temperature
​ Go Critical Temperature = (2*Stagnation Temperature)/(Specific Heat Ratio+1)
Isentropic Compressibility for given Density and Speed of Sound
​ Go Isentropic Compressibility = 1/(Density*Speed of Sound^2)
Mach Number
​ Go Mach Number = Speed of Object/Speed of Sound
Speed of Sound given Isentropic Change
​ Go Speed of Sound = sqrt(Isentropic Change)
Mach Angle
​ Go Mach Angle = asin(1/Mach Number)
Isentropic Change across Sound Wave
​ Go Isentropic Change = Speed of Sound^2

Speed of Sound Formula

Speed of Sound = sqrt(Specific Heat Ratio*[R-Dry-Air]*Static Temperature)
a = sqrt(γ*[R-Dry-Air]*Ts)

Which factors affect the speed of sound?

There are two factors that affect the speed of sound: The density of the medium and the Temperature of the medium.

How to Calculate Speed of Sound?

Speed of Sound calculator uses Speed of Sound = sqrt(Specific Heat Ratio*[R-Dry-Air]*Static Temperature) to calculate the Speed of Sound, The Speed of Sound, is the velocity at which small pressure disturbances, or sound waves, propagate through a medium. It represents the rate at which these disturbances travel through the medium, transferring energy and information. Speed of Sound is denoted by a symbol.

How to calculate Speed of Sound using this online calculator? To use this online calculator for Speed of Sound, enter Specific Heat Ratio (γ) & Static Temperature (Ts) and hit the calculate button. Here is how the Speed of Sound calculation can be explained with given input values -> 344.9012 = sqrt(1.4*[R-Dry-Air]*296).

FAQ

What is Speed of Sound?
The Speed of Sound, is the velocity at which small pressure disturbances, or sound waves, propagate through a medium. It represents the rate at which these disturbances travel through the medium, transferring energy and information and is represented as a = sqrt(γ*[R-Dry-Air]*Ts) or Speed of Sound = sqrt(Specific Heat Ratio*[R-Dry-Air]*Static Temperature). The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume of the flowing fluid for non-viscous and compressible flow & The Static Temperature is defined as the temperature measured by a thermometer placed within the fluid without affecting the fluid's velocity or pressure.
How to calculate Speed of Sound?
The Speed of Sound, is the velocity at which small pressure disturbances, or sound waves, propagate through a medium. It represents the rate at which these disturbances travel through the medium, transferring energy and information is calculated using Speed of Sound = sqrt(Specific Heat Ratio*[R-Dry-Air]*Static Temperature). To calculate Speed of Sound, you need Specific Heat Ratio (γ) & Static Temperature (Ts). With our tool, you need to enter the respective value for Specific Heat Ratio & Static Temperature 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 Speed of Sound?
In this formula, Speed of Sound uses Specific Heat Ratio & Static Temperature. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Speed of Sound = sqrt(Isentropic Change)
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