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Pressure At Upstream Point By Bernoulli's Equation Calculator

Bernoulli's Equation:

\[ P_1 = P_2 - 0.5 \times \rho \times (V_1^2 - V_2^2) \]

Pa
kg/m³
m/s
m/s

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1. What is Bernoulli's Equation?

Bernoulli's equation describes the relationship between pressure, velocity, and elevation in a fluid flow. It states that for an inviscid flow, an increase in fluid speed occurs simultaneously with a decrease in pressure or a decrease in the fluid's potential energy.

2. How Does the Calculator Work?

The calculator uses Bernoulli's equation:

\[ P_1 = P_2 - 0.5 \times \rho \times (V_1^2 - V_2^2) \]

Where:

Explanation: This equation calculates the pressure difference between two points in a fluid flow based on their velocity difference and fluid density.

3. Importance of Pressure Calculation

Details: Accurate pressure calculation is crucial for fluid dynamics analysis, pipe system design, aerodynamics, and various engineering applications where fluid flow is involved.

4. Using the Calculator

Tips: Enter pressure at point 2 in Pascals, fluid density in kg/m³, and velocities at both points in m/s. All values must be valid (density > 0, velocities ≥ 0).

5. Frequently Asked Questions (FAQ)

Q1: What are the assumptions of Bernoulli's equation?
A: The equation assumes steady flow, incompressible fluid, inviscid flow, and flow along a streamline.

Q2: When is Bernoulli's equation not applicable?
A: It's not applicable for viscous fluids, compressible flows, unsteady flows, or flows with significant heat transfer.

Q3: What are typical units for pressure in fluid dynamics?
A: Pascals (Pa) are the SI unit, but other common units include psi, bar, atm, and mmHg depending on the application.

Q4: How does elevation affect Bernoulli's equation?
A: The full Bernoulli equation includes elevation terms: \( P_1 + \frac{1}{2}\rho V_1^2 + \rho g h_1 = P_2 + \frac{1}{2}\rho V_2^2 + \rho g h_2 \)

Q5: Can this calculator be used for gases?
A: For low-speed gas flows where compressibility effects are negligible, the equation can provide reasonable approximations.

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