Stagnation pressure

In fluid dynamics, stagnation pressure (or pitot pressure) is the static pressure at a stagnation point in a fluid flow.^[1] At a stagnation point the fluid velocity is zero and all kinetic energy has been converted into pressure energy (isentropically). Stagnation pressure is equal to the sum of the free-stream dynamic pressure and free-stream static pressure.^[2]

Stagnation pressure is sometimes referred to as pitot pressure because it is measured using a pitot tube.

Magnitude

The magnitude of stagnation pressure can be derived from a simplified form of Bernoulli Equation.^[3]^[1] For incompressible flow,

P_{\text{stagnation}}={\tfrac {1}{2}}\rho v^{2}+P_{\text{static}}

where:

P_{\text{stagnation}}

is the stagnation pressure

\rho \;

is the fluid density

v

is the velocity of fluid

P_{\text{static}}

is the static pressure at any point.

At a stagnation point, the velocity of the fluid is zero. If the gravity head of the fluid at a particular point in a fluid flow is zero, then the stagnation pressure at that particular point is equal to total pressure.^[1] However, in general total pressure differs from stagnation pressure in that total pressure equals the sum of stagnation pressure and gravity head.

P_{\text{total}}=0+P_{\text{stagnation}}\;

In compressible flow the stagnation pressure is equal to total pressure only if the fluid entering the stagnation point is brought to rest isentropically.^[4] For many purposes in compressible flow, the stagnation enthalpy or stagnation temperature plays a role similar to the stagnation pressure in incompressible flow.

Compressible flow

Stagnation pressure is the static pressure a fluid retains when brought to rest isentropically from Mach number M.^[5]

{\frac {p_{t}}{p}}=\left(1+{\frac {\gamma -1}{2}}M^{2}\right)^{\frac {\gamma }{\gamma -1}}\,

or, assuming an isentropic process, the stagnation pressure can be calculated from the ratio of stagnation temperature to static temperature:

{\frac {p_{t}}{p}}=\left({\frac {T_{t}}{T}}\right)^{\frac {\gamma }{\gamma -1}}\,

where:

p_{t}

is the stagnation pressure

p

is the static pressure

T_{t}

is the stagnation temperature

T

is the static temperature

\gamma

ratio of specific heats

The above derivation holds only for the case when the fluid is assumed to be calorically perfect. For such fluids, specific heats and $\gamma$ are assumed to be constant and invariant with temperature (a thermally perfect fluid).

Notes

1 2 3 Clancy, L.J., Aerodynamics, Section 3.5
↑ Stagnation Pressure at Eric Weisstein's World of Physics (Wolfram Research)
↑ Equation 4, Bernoulli Equation - The Engineering Toolbox
↑ Clancy, L.J. Aerodynamics, Section 3.12
↑ Equations 35,44, Equations, Tables and Charts for Compressible Flow

References

Clancy, L.J. (1975), Aerodynamics, Pitman Publishing Limited, London. ISBN 0-273-01120-0
Cengel, Boles, "Thermodynamics, an engineering approach, McGraw Hill, ISBN 0-07-254904-1

External links

Pitot-Statics and the Standard Atmosphere
F. L. Thompson (1937) The Measurement of Air Speed in Airplanes, NACA Technical note #616, from SpaceAge Control.

This article is issued from Wikipedia - version of the 6/22/2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.