Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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Shikha Maurya
Indian Institute of Technology (IIT), Bombay
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11 Other formulas that you can solve using the same Inputs

Heat Loss due to Pipe
Heat Loss due to Pipe=(Force*Length*Fluid Velocity^2)/(2*Diameter *Acceleration Due To Gravity) GO
Reynolds Number for Circular Tubes
Reynolds Number=Density*Fluid Velocity*Diameter /Dynamic viscosity GO
Perimeter of a Semicircle when circumference of circle is given
Perimeter=(Circumference of Circle/2)+Diameter GO
Diameter of circumscribing sphere when diameter and height of circumscribed cylinder is known
Diameter of Sphere=sqrt(Diameter ^2+Height^2) GO
Cutting Speed
Cutting Speed=pi*Diameter *Angular Speed GO
Area of a Circle when diameter is given
Area of Circle=(pi/4)*Diameter ^2 GO
Perimeter of a quarter circle when diameter is given
Perimeter=Diameter *((pi/4)+1) GO
Perimeter of a Semicircle when diameter is given
Perimeter=Diameter *((pi/2)+1) GO
Area of a quarter circle when diameter is given
Area=(pi*(Diameter )^2)/16 GO
Area of a Semicircle when diameter is given
Area=(pi*(Diameter )^2)/8 GO
Radius of a circle when diameter is given
Radius=Diameter /2 GO

11 Other formulas that calculate the same Output

Coefficient of pressure with similarity parameters
Pressure coefficient=(2*(Flow Deflection angle)^2)*(((Specific Heat Ratio+1)/4)+sqrt((((Specific Heat Ratio+1)/4)^2)+(1/(Hypersonic similarity parameter)^2))) GO
Coefficient of pressure with slenderness ratio
Pressure coefficient=2*(Slenderness Ratio^2)*(Non-dimensionalized Pressure-(1/(Specific Heat Ratio*(Mach Number^2)*(Slenderness Ratio^2)))) GO
Pressure coefficient for slender bodies of revolution
Pressure coefficient=2*(Angle of Deflection^2)+(Curvature of the surface *Distance of Point from Centroidal Axis) GO
Pressure coefficient for slender 2-D bodies
Pressure coefficient=2*((deflection angle^2)+(Curvature of the surface *Distance of Point from Centroidal Axis)) GO
Exact relation for pressure coefficient behind an oblique shock wave
Pressure coefficient=(4/(Specific Heat Ratio+1))*(((sin(Wave angle))^2)-(1/Mach Number^2)) GO
Modified Newtonian Law
Pressure coefficient=The maximum pressure coefficient*(sin(deflection angle))^2 GO
Exact relation for pressure coefficient behind an oblique shock wave when Mach no. tends to infinite
Pressure coefficient=(4/(Specific Heat Ratio+1))*(sin(Wave angle))^2 GO
Supersonic expression for pressure coefficient on a surface with local deflection angle θ
Pressure coefficient=(2*deflection angle)/(sqrt(Mach Number^2-1)) GO
Non-dimensional pressure coefficient
Pressure coefficient=Change in static pressure/Dynamic Pressure GO
Newtonian sine-squared law for pressure coefficient
Pressure coefficient=2*(sin(deflection angle))^2 GO
Coefficient of pressure derived from oblique shock theory
Pressure coefficient=2*(sin(Wave angle))^2 GO

Pressure coefficient for Blunt-nosed cylinder: Formula

Pressure coefficient=0.096*(Drag Coefficient^(1/2))/(Distance from the nose tip to required base dia/Diameter )
C<sub>p</sub>=0.096*(C<sub>D</sub>^(1/2))/(x/d)
More formulas
Exact pressure coefficient for blast wave theory GO
Pressure coefficient for blast wave theory at very high values of mach GO
Pressure coefficient for Blunt-nosed plate: GO
Pressure coefficient combined with blast wave for the shuttle GO
Pressure coefficient combined with blast wave for the shuttle at angle of attack GO

What is coefficient of pressure?

The pressure coefficient is a dimensionless number which describes the relative pressures throughout a flow field in fluid dynamics.

How to Calculate Pressure coefficient for Blunt-nosed cylinder:?

Pressure coefficient for Blunt-nosed cylinder: calculator uses Pressure coefficient=0.096*(Drag Coefficient^(1/2))/(Distance from the nose tip to required base dia/Diameter ) to calculate the Pressure coefficient, Pressure coefficient for Blunt-nosed cylinder: formula is defined as the inter relation between drag coefficient, distance from the tip of the blunt nose and base diameter . Pressure coefficient and is denoted by Cp symbol.

How to calculate Pressure coefficient for Blunt-nosed cylinder: using this online calculator? To use this online calculator for Pressure coefficient for Blunt-nosed cylinder:, enter Drag Coefficient (CD), Distance from the nose tip to required base dia (x) and Diameter (d) and hit the calculate button. Here is how the Pressure coefficient for Blunt-nosed cylinder: calculation can be explained with given input values -> 0.96 = 0.096*(100^(1/2))/(10/10).

FAQ

What is Pressure coefficient for Blunt-nosed cylinder:?
Pressure coefficient for Blunt-nosed cylinder: formula is defined as the inter relation between drag coefficient, distance from the tip of the blunt nose and base diameter and is represented as Cp=0.096*(CD^(1/2))/(x/d) or Pressure coefficient=0.096*(Drag Coefficient^(1/2))/(Distance from the nose tip to required base dia/Diameter ). Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water, Distance from the nose tip to required base dia, used for studying the leading edge of the hypersonic vehicles and Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.
How to calculate Pressure coefficient for Blunt-nosed cylinder:?
Pressure coefficient for Blunt-nosed cylinder: formula is defined as the inter relation between drag coefficient, distance from the tip of the blunt nose and base diameter is calculated using Pressure coefficient=0.096*(Drag Coefficient^(1/2))/(Distance from the nose tip to required base dia/Diameter ). To calculate Pressure coefficient for Blunt-nosed cylinder:, you need Drag Coefficient (CD), Distance from the nose tip to required base dia (x) and Diameter (d). With our tool, you need to enter the respective value for Drag Coefficient, Distance from the nose tip to required base dia and Diameter 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 coefficient?
In this formula, Pressure coefficient uses Drag Coefficient, Distance from the nose tip to required base dia and Diameter . We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Pressure coefficient=Change in static pressure/Dynamic Pressure
  • Pressure coefficient=(4/(Specific Heat Ratio+1))*(((sin(Wave angle))^2)-(1/Mach Number^2))
  • Pressure coefficient=(4/(Specific Heat Ratio+1))*(sin(Wave angle))^2
  • Pressure coefficient=(2*(Flow Deflection angle)^2)*(((Specific Heat Ratio+1)/4)+sqrt((((Specific Heat Ratio+1)/4)^2)+(1/(Hypersonic similarity parameter)^2)))
  • Pressure coefficient=2*(sin(deflection angle))^2
  • Pressure coefficient=(2*deflection angle)/(sqrt(Mach Number^2-1))
  • Pressure coefficient=The maximum pressure coefficient*(sin(deflection angle))^2
  • Pressure coefficient=2*((deflection angle^2)+(Curvature of the surface *Distance of Point from Centroidal Axis))
  • Pressure coefficient=2*(Angle of Deflection^2)+(Curvature of the surface *Distance of Point from Centroidal Axis)
  • Pressure coefficient=2*(sin(Wave angle))^2
  • Pressure coefficient=2*(Slenderness Ratio^2)*(Non-dimensionalized Pressure-(1/(Specific Heat Ratio*(Mach Number^2)*(Slenderness Ratio^2))))
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