Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Rushi Shah
K J Somaiya College of Engineering (K J Somaiya), Mumbai
Rushi Shah has verified this Calculator and 100+ more calculators!

11 Other formulas that you can solve using the same Inputs

Calorie Burn Rate
Calorie Burn Rate=(Weight*Sleeping*Time)+(Weight*Watching TV*Time)+(Weight*Typing Writing Desk Work*Time)+(Weight*Walking Very Slow 1.7 Mph)+(Weight*Walking 2.5 mph*Time)+(Weight*Bicycling Very Slow 50 Watts*Time)+(Weight*Walking 3 Mph*Time)+(Weight*Calisthenics Home Exercises*Time)+(Weight*Walking 3.4 Mph*Time)+(Weight*Bicycling Stationary*Time)+(Weight*Jogging *Time)+(Weight*Heavy Calisthenics*Time)+(Weight*Running Jogging In Place*Time)+(Weight*Rope Jumping*Time) GO
Propeller Efficiency for given Endurance of Propeller-Driven Airplane
Propeller efficiency=Endurance of aircraft/((1/Specific Fuel Consumption)*((lift coefficient^1.5)/Drag Coefficient)*(sqrt(2*Freestream density*Reference Area))*(((1/Gross Weight)^(1/2))-((1/Weight without fuel)^(1/2)))) GO
Specific Fuel Consumption for given Endurance of Propeller-Driven Airplane
Specific Fuel Consumption=(Propeller efficiency/Endurance of aircraft)*((lift coefficient^1.5)/Drag Coefficient)*(sqrt(2*Freestream density*Reference Area))*(((1/Gross Weight)^(1/2))-((1/Weight without fuel)^(1/2))) GO
Endurance of Propeller-Driven Airplane
Endurance of aircraft=(Propeller efficiency/Specific Fuel Consumption)*((lift coefficient^1.5)/Drag Coefficient)*(sqrt(2*Freestream density*Reference Area))*(((1/Gross Weight)^(1/2))-((1/Weight without fuel)^(1/2))) GO
Heart Rate Based Calorie Burn For Male
Heart Rate Based Calorie Burn For Male=((-55.0969+(0.6309*Heart Rate)+(0.1988*Weight)+(0.2017*Age))/4.184)*60*Time GO
Wave Number Of A Moving Particle
Wave Number=Energy/(Plancks Constant*Velocity Of Light in Vacuum) GO
Wavelength Of A Moving Particle
Wavelength=(Plancks Constant*Velocity Of Light in Vacuum)/Energy GO
Non- dimensionalised time
Non dimensionalized time=Time/(Length/Freestream Velocity) GO
Distance from tip of the leading edge to the base
Distance from X-axis=Freestream Velocity*Time GO
Heat generated through resistance
Heat Rate=Electric Current^2*Resistance*Time GO
Frequency Of A Moving Particle
frequency=Energy/Plancks Constant GO

11 Other formulas that calculate the same Output

New pressure after the shock formation for compression wave
Pressure=density ahead of shock*(1+((Specific Heat Ratio-1)/2)*(Normal velocity/Old speed of sound))^(2*Specific Heat Ratio/(Specific Heat Ratio-Time)) GO
Modified pressure equation for cylindrical blast wave
Pressure=[BoltZ]*Freestream density*(sqrt(pi/8))*Diameter *(sqrt(Drag Coefficient))*(Freestream Velocity^2/Distance from X-axis) GO
formula For creation pressure for the planar blast wave
Pressure=[BoltZ]*Freestream density*((Energy/Freestream density)^(2/3))*(Time)^(-2/3) GO
Pressure when Resultant is Outside Middle Third
Pressure=2*Total downward force on soil/(3*middle third distance) GO
Pressure of the liquid entering the motor
Pressure=Theoretical torque/Theoretical volumetric displacement GO
Pressure
Pressure=(1/3)*Density of Gas*(Root mean square velocity)^2 GO
Pressure when density and height are given
Pressure=Density*Acceleration Due To Gravity*Height GO
Pressure during retraction
Pressure=Force/(Area of piston-Area of piston rod) GO
Pressure in Excess of Atmospheric Pressure
Pressure=(specific weight of liquid)*(Height) GO
Pressure exerted
Pressure=Force/Area of piston GO
Pressure when force and area are given
Pressure=Force/Area GO

Pressure for the cylindrical blast wave Formula

Pressure=Boltzmann constant 1*Freestream density*((Energy/Freestream density)^(1/2))/(Time)
P=kB1*ρ<sub>∞</sub>*((e/ρ<sub>∞</sub>)^(1/2))/(t)
More formulas
Boltzmann constant for cylindrical blast wave GO
formula For creation pressure for the planar blast wave GO
Radial coordinate of cylindrical blast wave GO
Radial coordinate for the planar blast wave, GO
Energy for the blast wave GO
Time required for the blast wave GO
Modified pressure equation for cylindrical blast wave GO
Pressure ratio for blunt cylinder blast wave GO
Simplified pressure ratio for blunt cylinder blast wave GO
Modified Radial coordinate equation for cylindrical blast wave GO
Modified Energy for the cylindrical blast wave GO
Coefficient of drag equation using energy released from blast wave GO
Pressure ratio for blunt slab blast wave GO
Radial coordinate of blunt slab blast wave GO
Blunt-nosed flat plate pressure ratio (first approximation) GO

What is Boltzmann constant?

The Boltzmann constant (kB or k) is the proportionality factor that relates the average relative kinetic energy of particles in a gas with the thermodynamic temperature of the gas

How to Calculate Pressure for the cylindrical blast wave?

Pressure for the cylindrical blast wave calculator uses Pressure=Boltzmann constant 1*Freestream density*((Energy/Freestream density)^(1/2))/(Time) to calculate the Pressure, The pressure for the cylindrical blast wave formula is defined as interrelation between Boltzmann constant, free stream density,energy and time. Pressure and is denoted by P symbol.

How to calculate Pressure for the cylindrical blast wave using this online calculator? To use this online calculator for Pressure for the cylindrical blast wave, enter Boltzmann constant 1 (kB1), Freestream density ), Energy (e) and Time (t) and hit the calculate button. Here is how the Pressure for the cylindrical blast wave calculation can be explained with given input values -> 7.686E-5 = 1*1.225*((1/1.225)^(1/2))/(14400).

FAQ

What is Pressure for the cylindrical blast wave?
The pressure for the cylindrical blast wave formula is defined as interrelation between Boltzmann constant, free stream density,energy and time and is represented as P=kB1*ρ*((e/ρ)^(1/2))/(t) or Pressure=Boltzmann constant 1*Freestream density*((Energy/Freestream density)^(1/2))/(Time). The Boltzmann constant 1 is the The Boltzmann constant used for cylindrical blast wave in hypersonic blast theory, Freestream density is the mass per unit volume of air far upstream of an aerodynamic body at a given altitude, Energy is the amount of work done and Time can be defined as the ongoing and continuous sequence of events that occur in succession, from the past through the present to the future.
How to calculate Pressure for the cylindrical blast wave?
The pressure for the cylindrical blast wave formula is defined as interrelation between Boltzmann constant, free stream density,energy and time is calculated using Pressure=Boltzmann constant 1*Freestream density*((Energy/Freestream density)^(1/2))/(Time). To calculate Pressure for the cylindrical blast wave, you need Boltzmann constant 1 (kB1), Freestream density ), Energy (e) and Time (t). With our tool, you need to enter the respective value for Boltzmann constant 1, Freestream density, Energy and Time 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 Pressure?
In this formula, Pressure uses Boltzmann constant 1, Freestream density, Energy and Time. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Pressure=Force/Area
  • Pressure=Density*Acceleration Due To Gravity*Height
  • Pressure=(specific weight of liquid)*(Height)
  • Pressure=(1/3)*Density of Gas*(Root mean square velocity)^2
  • Pressure=2*Total downward force on soil/(3*middle third distance)
  • Pressure=Theoretical torque/Theoretical volumetric displacement
  • Pressure=Force/Area of piston
  • Pressure=Force/(Area of piston-Area of piston rod)
  • Pressure=[BoltZ]*Freestream density*((Energy/Freestream density)^(2/3))*(Time)^(-2/3)
  • Pressure=[BoltZ]*Freestream density*(sqrt(pi/8))*Diameter *(sqrt(Drag Coefficient))*(Freestream Velocity^2/Distance from X-axis)
  • Pressure=density ahead of shock*(1+((Specific Heat Ratio-1)/2)*(Normal velocity/Old speed of sound))^(2*Specific Heat Ratio/(Specific Heat Ratio-Time))
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