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I'm not sure if a fluid flow (in general unsteady) is in thermodynamic equilibrium (say flow in a channel which has a pressure gradient) and so would the static pressure at a point in the channel be different from the thermodynamic pressure? The dynamic pressure is the difference between the total pressure—that is, the pressure you would actually measure at the given point in the moving fluid, with some appropriate instrument—and the static pressure To the best of my knowledge the total pressure can be only measure if we bring the fluid to rest, e.g 10 what is basically the difference between static pressure and dynamic pressure
While studying bernoulli's theorem, i came before these terms When the fluid flows through a small area, its pressure energy decreases & kinetic energy increases and vice versa. Total pressure in bernoulli's equation is often defined as the sum of static and dynamic pressure, excluding gravitational potential energy (gpe) terms The discussion highlights a confusion regarding the treatment of total pressure at different points in a hot air balloon, where static pressure varies with altitude while the total pressure appears constant under certain assumptions
Its same like a rubber band is stretched from all the points outwards so a stress is developed in it Static pressure is defined as the pressure exerted by a fluid at rest, influenced by external factors such as atmospheric pressure It is distinct from hydrostatic pressure, which specifically relates to the weight of the fluid above a given point and increases with depth The bernoulli equation incorporates static pressure, hydrostatic pressure, and dynamic pressure, illustrating the.
I have trouble understanding what exactly is total pressure In bernoulli's equation, total pressure seems to be the sum of the static, dynamic, and gravitational potential term If i apply that definition, i will come to the conclusion that total pressure at a, b, c, and d is equal, while static pressure varies depending on. The discussion centers on understanding the relationship between static and dynamic pressure as described by bernoulli's equation
As airflow speed increases, static pressure decreases due to conservation of energy. I looked at many definitions of total pressure which states that it is the sum of static pressure and dynamic pressure However, the full form of bernoulli's equation includes the potential term ρg. Logically, the total pressure is then equal to the static pressure
However, the total pressure is also called the stagnation pressure, yet it can be measured anywhere, not just at stagnation points Why do we then also refer to total pressure as stagnation pressure, as in this article?
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