Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
Maiarutselvan V has verified this Calculator and 200+ more calculators!

11 Other formulas that you can solve using the same Inputs

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
Pressure ratio for blunt cylinder blast wave
pressure ratio=0.8773*[BoltZ]*(Mach Number^2)*(sqrt(Drag Coefficient))*(Distance from X-axis/Diameter ^(-1)) GO
Pressure ratio for blunt slab blast wave
pressure ratio=0.127*(Mach Number^2)*(Drag Coefficient^(2/3))*((Distance from X-axis/Diameter )^(-2/3)) GO
Radial coordinate of Blunt-nosed cylinder (first approximation):
Radial coordinate=0.795*Diameter *(Drag Coefficient^(1/4))*((Distance from X-axis/Diameter )^(1/2)) GO
Radial coordinate of blunt slab blast wave
Radial coordinate=0.794*Diameter *(Drag Coefficient^(1/3))*((Distance from X-axis/Diameter )^(2/3)) GO
Blunt-nosed flat plate pressure ratio (first approximation)
pressure ratio=0.121*(Mach Number^2)*((Drag Coefficient/(Distance from X-axis/Diameter ))^(2/3)) GO
Modified Radial coordinate equation for cylindrical blast wave
Radial coordinate=0.792*Diameter *(Drag Coefficient^(1/4))*sqrt(Distance from X-axis/Diameter ) GO
Simplified pressure ratio for blunt cylinder blast wave
pressure ratio=0.0681*(Mach Number^2)*sqrt(Drag Coefficient)/(Distance from X-axis/Diameter ) GO
Pressure ratio of Blunt-nosed cylinder (first approximation):
pressure ratio=0.067*(Mach Number^2)*sqrt(Drag Coefficient)/(Distance from X-axis/Diameter ) GO
Blunt-nosed radial coordinate flat plate (first approximation):
Radial coordinate=0.774*(Drag Coefficient^(1/3))*((Distance from X-axis/Diameter )^(2/3)) GO
Time required for the blast wave
Time=Distance from X-axis/Freestream Velocity GO

1 Other formulas that calculate the same Output

curvilinear grid location equation
Grid points=(Distance from Y-axis-local ordinate of the body)/local shock-layer thickness GO

Grid point calculation for shock waves Formula

Grid points=(Distance from X-axis-Body shape in hypersonic flow)/Local shock-detachment distance
ζ=(y-b)/𝛿
More formulas
Mach wave behind the shock GO
Mach wave behind the shock with mach infinity GO
Local shock velocity equation GO
Pressure ratio for unsteady waves GO
Pressure ratio for unsteady waves with subtracted induced mass motion for expansion waves GO
Temperature ratio for unsteady compression waves GO
Temperature ratio for unsteady expansion wave GO
New pressure after the shock formation for compression wave GO
New pressure after the shock formation, subtracted to velocity for expansion wave GO
Density before shock formation for compression wave GO
Density before the shock formation for expansion wave GO
Ratio of new and old temperature GO
Ratio of new and old temperature for expansion waves GO
Detachment distance of sphere cone GO
Nose radius of sphere cone GO
Detachment distance of cylinder-wedge GO
Nose radius of cylinder-wedge GO

what is a shock wave?

Shock wave, strong pressure wave in any elastic medium such as air, water, or a solid substance, produced by supersonic aircraft, explosions, lightning, or other phenomena that create violent changes in pressure.

How to Calculate Grid point calculation for shock waves?

Grid point calculation for shock waves calculator uses Grid points=(Distance from X-axis-Body shape in hypersonic flow)/Local shock-detachment distance to calculate the Grid points, The Grid point calculation for shock waves formula is defined as the ratio of the distance from the origin of shock along the x-axis minus the body shape to the detachment distance of shock wave. Grid points and is denoted by ζ symbol.

How to calculate Grid point calculation for shock waves using this online calculator? To use this online calculator for Grid point calculation for shock waves, enter Distance from X-axis (y), Body shape in hypersonic flow (b) and Local shock-detachment distance (𝛿) and hit the calculate button. Here is how the Grid point calculation for shock waves calculation can be explained with given input values -> 0 = (0.01-0.01)/0.001.

FAQ

What is Grid point calculation for shock waves?
The Grid point calculation for shock waves formula is defined as the ratio of the distance from the origin of shock along the x-axis minus the body shape to the detachment distance of shock wave and is represented as ζ=(y-b)/𝛿 or Grid points=(Distance from X-axis-Body shape in hypersonic flow)/Local shock-detachment distance. Distance from X-axis is defined as the distance from the point where stress is to be computed to XX axis, Body shape in hypersonic flow. is the shape of the shock wave and Local shock-detachment distance , is the distance of shock formation from leading edge.
How to calculate Grid point calculation for shock waves?
The Grid point calculation for shock waves formula is defined as the ratio of the distance from the origin of shock along the x-axis minus the body shape to the detachment distance of shock wave is calculated using Grid points=(Distance from X-axis-Body shape in hypersonic flow)/Local shock-detachment distance. To calculate Grid point calculation for shock waves, you need Distance from X-axis (y), Body shape in hypersonic flow (b) and Local shock-detachment distance (𝛿). With our tool, you need to enter the respective value for Distance from X-axis, Body shape in hypersonic flow and Local shock-detachment distance 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 Grid points?
In this formula, Grid points uses Distance from X-axis, Body shape in hypersonic flow and Local shock-detachment distance. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Grid points=(Distance from Y-axis-local ordinate of the body)/local shock-layer thickness
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