Stagnation Pressure Solution

STEP 0: Pre-Calculation Summary
Formula Used
Stagnation Pressure = 2*Dynamic Pressure*(cos(Newtonian angle))^2+Free Stream Pressure
p' = 2*Pdynamic*(cos(Φ))^2+p
This formula uses 1 Functions, 4 Variables
Functions Used
cos - Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle., cos(Angle)
Variables Used
Stagnation Pressure - (Measured in Pascal) - Stagnation Pressure is the pressure at the stagnation temperature during the process of ramming.
Dynamic Pressure - (Measured in Pascal) - Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.
Newtonian angle - (Measured in Radian) - Newtonian angle is the angle between the normal to the surface and the freestream.
Free Stream Pressure - (Measured in Pascal) - Free Stream Pressure is the pressure of fluid that hasn't encountered any disturbance.
STEP 1: Convert Input(s) to Base Unit
Dynamic Pressure: 12.56 Pascal --> 12.56 Pascal No Conversion Required
Newtonian angle: 56 Radian --> 56 Radian No Conversion Required
Free Stream Pressure: 7.9 Pascal --> 7.9 Pascal No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
p' = 2*Pdynamic*(cos(Φ))^2+p --> 2*12.56*(cos(56))^2+7.9
Evaluating ... ...
p' = 26.1869719518201
STEP 3: Convert Result to Output's Unit
26.1869719518201 Pascal --> No Conversion Required
FINAL ANSWER
26.1869719518201 26.18697 Pascal <-- Stagnation Pressure
(Calculation completed in 00.020 seconds)

Credits

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Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
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Verified by Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
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Laminar Boundary Layer at Stagnation point on Blunt body Calculators

Stagnation Pressure
​ LaTeX ​ Go Stagnation Pressure = 2*Dynamic Pressure*(cos(Newtonian angle))^2+Free Stream Pressure
Nusselt Number for Stagnation Point on Blunt Body
​ LaTeX ​ Go Nusselt Number = Nusselt Number at Stagnation Point*(0.7*(cos(Newtonian angle))^(1.5)+0.3)
Newtonian Dynamic Pressure
​ LaTeX ​ Go Dynamic Pressure = 0.5*(Stagnation Pressure-Free Stream Pressure)
Newtonian Pressure Distribution over Surface using Cosine Angle
​ LaTeX ​ Go Pressure Coefficient = 2*(cos(Newtonian angle))^2

Stagnation Pressure Formula

​LaTeX ​Go
Stagnation Pressure = 2*Dynamic Pressure*(cos(Newtonian angle))^2+Free Stream Pressure
p' = 2*Pdynamic*(cos(Φ))^2+p

What is Newtonian pressure distribution?

Newtonian Theory uses the pressure distribution of air flowing over a body to calculate forces and moments at hypersonic speeds.

How to Calculate Stagnation Pressure?

Stagnation Pressure calculator uses Stagnation Pressure = 2*Dynamic Pressure*(cos(Newtonian angle))^2+Free Stream Pressure to calculate the Stagnation Pressure, The Stagnation pressure formula is defined as the interrelation between dynamic pressure, cosine angle between normal to the surface, and free stream flow and freestream static pressure. Stagnation Pressure is denoted by p' symbol.

How to calculate Stagnation Pressure using this online calculator? To use this online calculator for Stagnation Pressure, enter Dynamic Pressure (Pdynamic), Newtonian angle (Φ) & Free Stream Pressure (p) and hit the calculate button. Here is how the Stagnation Pressure calculation can be explained with given input values -> 76.18697 = 2*12.56*(cos(56))^2+7.9.

FAQ

What is Stagnation Pressure?
The Stagnation pressure formula is defined as the interrelation between dynamic pressure, cosine angle between normal to the surface, and free stream flow and freestream static pressure and is represented as p' = 2*Pdynamic*(cos(Φ))^2+p or Stagnation Pressure = 2*Dynamic Pressure*(cos(Newtonian angle))^2+Free Stream Pressure. Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid, Newtonian angle is the angle between the normal to the surface and the freestream & Free Stream Pressure is the pressure of fluid that hasn't encountered any disturbance.
How to calculate Stagnation Pressure?
The Stagnation pressure formula is defined as the interrelation between dynamic pressure, cosine angle between normal to the surface, and free stream flow and freestream static pressure is calculated using Stagnation Pressure = 2*Dynamic Pressure*(cos(Newtonian angle))^2+Free Stream Pressure. To calculate Stagnation Pressure, you need Dynamic Pressure (Pdynamic), Newtonian angle (Φ) & Free Stream Pressure (p). With our tool, you need to enter the respective value for Dynamic Pressure, Newtonian angle & Free Stream Pressure and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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