Suraj Kumar
Birsa Institute of Technology (BIT), Sindri
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Ishita Goyal
Meerut Institute of Engineering and Technology (MIET), Meerut
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11 Other formulas that you can solve using the same Inputs

Deflection for Hollow Rectangle When Load in Middle
Deflection of Beam=(Greatest Safe Load*Length of the Beam^3)/(32*(Sectional Area*(Depth of the Beam^2)-Interior Cross-Sectional Area of Beam*(Interior Depth of the Beam^2))) GO
Deflection for Hollow Rectangle When Load is Distributed
Deflection of Beam=Greatest Safe Load*(Length of the Beam^3)/(52*(Sectional Area*Depth of the Beam^-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam^2)) GO
Greatest Safe Load for Hollow Rectangle When Load is Distributed
Greatest Safe Load=1780*(Sectional Area*Depth of the Beam-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam)/Distance between Supports GO
Greatest Safe Load for Hollow Rectangle When Load in Middle
Greatest Safe Load=(890*(Sectional Area*Depth of the Beam-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam))/Length of the Beam GO
Deflection for Solid Rectangle When Load is Distributed
Deflection of Beam=(Greatest safe distributed load*Length of the Beam^3)/(52*Sectional Area*Depth of the Beam^2) GO
Deflection for Solid Rectangle When Load in Middle
Deflection of Beam=(Greatest Safe Load*Length of the Beam^3)/(32*Sectional Area*Depth of the Beam^2) GO
Pressure at BC
Pressure at BC=((Compressive force*sin(Oblique angle)*tan(Oblique angle/2))/Sectional Area) GO
Greatest Safe Load for Solid Rectangle When Load is Distributed
Greatest safe distributed load=1780*Sectional Area*Depth of the Beam/Length of the Beam GO
Greatest Safe Load for Solid Cylinder When Load is Distributed
Greatest Safe Load=1333*(Sectional Area*Depth of the Beam)/Length of the Beam GO
Greatest Safe Load for Solid Cylinder When Load in Middle
Greatest Safe Load=(667*Sectional Area*Depth of the Beam)/Length of the Beam GO
Greatest Safe Load for Solid Rectangle When Load in Middle
Greatest Safe Load=890*Sectional Area*Depth of the Beam/Length of the Beam GO

Pressure at AC Formula

Pressure at AC=((Compressive force*sin(Oblique angle))/(Sectional Area*tan(Oblique angle/2)))
f<sub>1</sub>=((F*sin(φ))/(A*tan(φ/2)))
More formulas
Extreme Fiber Stress in Bending for a Rectangular Timber Beam GO
Extreme Fiber Stress for a Rectangular Timber Beam when Section Modulus is Given GO
Section Modulus GO
Bending Moment when Extreme Fiber Stress for a Rectangular Timber Beam is Given GO
Beam Width when Extreme Fiber Stress for a Rectangular Timber Beam is Given GO
Beam Depth when Extreme Fiber Stress for a Rectangular Timber Beam is Given GO
Horizontal Shearing Stress in a Rectangular Timber Beam GO
Total Shear when Horizontal Shearing Stress is Given GO
Beam Width when Horizontal Shearing Stress is Given GO
Beam Depth when Horizontal Shearing Stress is Given GO
Horizontal Shearing Stress in a Rectangular Timber Beam when Notch in the Lower Face GO
Modified Total End Shear for Uniform Loading GO
Modified Total End Shear for Concentrated Loads GO
Elasticity Modulus when Allowable Unit Stress on Timber Columns for a Single Member is Given GO
Allowable Unit Stress on Timber Columns for a Single Member GO
Allowable Unit Stress on Timber Columns of Square or Rectangular Cross Section GO
Elasticity Modulus when Allowable Unit Stress of Square or Rectangular Timber Columns is Given GO
Allowable Unit Stress on Timber Columns of Circular Cross Section GO
Elasticity Modulus when Allowable Unit Stress of Circular Timber Columns is Given GO
Allowable Unit Stress at Angle to Grain GO
Allowable Compressive Stress Parallel to Grain for Short Columns GO
Allowable Compressive Stress Parallel to Grain for Intermediate Columns GO
Allowable Compressive Stress Parallel to Grain for Long Columns GO
Allowable Compressive Stress in a Rectangular Section GO
Elasticity Modulus when Allowable Compressive Stress in a Rectangular Section is Given GO
Allowable Compressive Stress Inclined to Grain GO
Pressure at BC GO
Adjusted Design Value for Extreme Fiber Bending GO
Adjusted Design Value for Tension GO
Adjusted Design Value for Shear GO
Adjusted Design Value for Compression Perpendicular to Grain GO
Adjusted Design Value for Compression Parallel to Grain GO
Adjusted Design Value for End Grain in Bearing Parallel to Grain GO
Adjusted Design Value for Lateral Loading for Bolts GO
Adjusted Value for Loading Parallel to Grain for Split Ring and Shear Plate Connectors GO
Adjusted Value for Loading Normal to Grain for Split Ring and Shear Plate Connectors GO
Adjusted Design Value for Withdrawal for Nails and Spikes GO
Adjusted Design Value for Lateral Loading for Nails and Spikes GO
Adjusted Design Value for Withdrawal for Wood Screws GO
Adjusted Design Value for Lateral Loading for Wood Screws GO
Adjusted Design Value for Withdrawal for Lag Screws GO
Adjusted Design Value for Lateral Loading for Lag Screws GO
Adjusted Design Value for Lateral Loading for Metal Plate Connectors GO
Adjusted Design Value for Withdrawal for Drift Bolts and Pins GO
Adjusted Design Value for Lateral Loading for Drift Bolts and Pins GO
Adjusted Design Value for Lateral Loading for Spike Grids GO
Factor for Multiplying Stresses and Deflections under Existing Loads GO
Maximum Compressive Stress for Uniaxial Bending GO
Maximum Compressive Stress for Biaxial Bending GO
Maximum Bending Stress for Load Applied to Narrow Member Face GO
Ultimate Unit Load GO
Allowable Unit Load for Hemlock Lumber GO
Allowable Unit Load for Longleaf Yellow Pine Lumber GO
Allowable Unit Load for Southern Cypress Lumber GO
Allowable Unit Load for Douglas Fir Lumber GO

What is pressure ?

Pressure is defined as the physical force exerted on an object. The force applied is perpendicular to the surface of objects per unit area.

How to Calculate Pressure at AC?

Pressure at AC calculator uses Pressure at AC=((Compressive force*sin(Oblique angle))/(Sectional Area*tan(Oblique angle/2))) to calculate the Pressure at AC, The Pressure at AC formula is defined as net normal force per unit area of face AC which can be calculated by compressive force , area and oblique angle. Pressure at AC and is denoted by f1 symbol.

How to calculate Pressure at AC using this online calculator? To use this online calculator for Pressure at AC, enter Compressive force (F), Oblique angle (φ) and Sectional Area (A) and hit the calculate button. Here is how the Pressure at AC calculation can be explained with given input values -> 1852.215 = ((7*sin(45))/(0.00645160000005161*tan(45/2))).

FAQ

What is Pressure at AC?
The Pressure at AC formula is defined as net normal force per unit area of face AC which can be calculated by compressive force , area and oblique angle and is represented as f1=((F*sin(φ))/(A*tan(φ/2))) or Pressure at AC=((Compressive force*sin(Oblique angle))/(Sectional Area*tan(Oblique angle/2))). Compressive force acting on the timber member, Oblique angle made by the line of action of force and Sectional Area is the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to the axis of the beam at a point.
How to calculate Pressure at AC?
The Pressure at AC formula is defined as net normal force per unit area of face AC which can be calculated by compressive force , area and oblique angle is calculated using Pressure at AC=((Compressive force*sin(Oblique angle))/(Sectional Area*tan(Oblique angle/2))). To calculate Pressure at AC, you need Compressive force (F), Oblique angle (φ) and Sectional Area (A). With our tool, you need to enter the respective value for Compressive force, Oblique angle and Sectional Area and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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