Unbalanced Thrust Force due to Internal Pressure
Unbalanced Thrust Force due to Internal Pressure (Unrestrained Straight Pipe) formula
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\( F \;=\; p \cdot A_c \) (Unrestrained Straight Pipe) \( p \;=\; \dfrac{ F }{ A_c }\) \( A_c \;=\; \dfrac{ F }{ p }\) |
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| Symbol | English | Metric |
| \( F \) = Internal Thrust Force | \(lbf\) | \(N\) |
| \( p \) = Internal Pressure | \(lbf \;/\; in^2\) | \(Pa\) |
| \( A_c \) = Area Cross-section of Pipe | \(in^2\) | \(mm^2\) |
Unbalanced thrust force due to internal pressure, abbreviated as \(F\) or \(T\), is the net axial force that acts on a component, such as a pipe, valves, fittings, or expansion joint, when the internal fluid pressure does not act equally in all opposing directions. In a straight, uniform pipe the pressure forces on opposite cross-sections balance each other, producing no net thrust. However, when there is a change in geometry, flow direction, or cross-sectional area, the pressure forces become unequal. This imbalance results in a thrust force that tends to push or pull the component along the direction of flow. The magnitude of the unbalanced thrust force depends on the internal pressure and the effective area over which the pressure acts, and it must be resisted by anchors, supports, or restraints to prevent excessive movement, structural damage, or failure of the piping system.

Unbalanced Thrust Force due to Internal Pressure (Pipe Bend) formula
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\( F \;=\; 2 \cdot p \cdot A_c \cdot sin\left( \dfrac{ \theta }{ 2 } \right) \) (Pipe Bend) \( p \;=\; \dfrac{ F }{ 2 \cdot A_c \cdot sin\left( \dfrac{ \theta }{ 2 } \right) } \) \( A_c \;=\; \dfrac{ F }{ 2 \cdot p \cdot sin\left( \dfrac{ \theta }{ 2 } \right) } \) |
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| Symbol | English | Metric |
| \( F \) = Resultant Thrust Force | \(lbf\) | \(N\) |
| \( p \) = Internal Pressure | \(lbf \;/\; in^2\) | \(Pa\) |
| \( A_c \) = Area Cross-section of Pipe | \(in^2\) | \(mm^2\) |
| \( \theta \) = Pipe Bend Angle | \(deg\) | \(rad\) |
Unbalanced Thrust Force due to Internal Pressure (Reducers) formula
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\( F \;=\; p \cdot \left( A_l - A_s \right) \) (Reducers) \( p \;=\; \dfrac{ F }{ A_l - A_s } \) \( A_l \;=\; \dfrac{ F }{ p } + A_s \) \( A_s \;=\; A_l - \dfrac{ F }{ p } \) |
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| Symbol | English | Metric |
| \( F \) = InternalThrust Force | \(lbf\) | \(N\) |
| \( p \) = Internal Pressure | \(lbf \;/\; in^2\) | \(Pa\) |
| \( A_l \) = Area Cross-section of Large End | \(in\) | \(mm\) |
| \( A_s \) = Area Cross-section of Small End | \(in\) | \(mm\) |
