There is one limitation to the Bernoulli equation : the equation cannot be applied to fluid passing through the wind turbine.
12.
More advanced forms may be applied to compressible flows at higher Mach numbers ( see the derivations of the Bernoulli equation ).
13.
These include fluid statics, fluid flows, e . g . laminar flow vs . turbulent flow, the Bernoulli equation.
14.
:Depending on what assumptions you're making, this problem can more easily be solved by one of the Bernoulli equations.
15.
In other words, the Bernoulli equations up and downstream of the rotor are the same as the Bernoulli expressions in the Betz model.
16.
The inlet gas stream enters the converging section and, as the area decreases, gas velocity increases ( in accordance with the Bernoulli equation ).
17.
The Bernoulli equation shows that the static pressure is highest when the velocity is zero and hence static pressure is at its maximum value at stagnation points.
18.
An exception to this rule is radiative shocks, which violate the assumptions leading to the Bernoulli equation, namely the lack of additional sinks or sources of energy.
19.
In 1753, Leonhard Euler showed how a theoretical trajectories might be calculated using his method as applied to the Bernoulli equation, but only for resistance varying as the square of the velocity.
20.
That would be on the same order of magnitude as the pressure drop predicted by the Bernoulli equation, no ? Preceding talk ) 19 : 55, 14 September 2012 ( UTC)
