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    Diameter Change in Compression Spring Calculator
    When a helical compression spring is compressed, an increase in the outside diameter occurs because the angularity of the coils changes so that it is nearly at a right angle to the axis.
    Short Rectangular Membrane Stress and Deflection Calculator
    The stress at various locations on short rectangular membranes are given by following equations and calculator
    Long Rectangular Membrane Design Calculator and Equations
    Long Rectangular Membrane Stress and Deflection Design Calculator and Equations
    Circular Membrane Stress and Deflection Calculator and Equations
    A membrane may be defined as a plate that is so thin that it may ne considered to have no bending rigidity. The only stresses present are in the plane of the surface and are uniform throughout the thickness of the membrane.
    Press Fit Bushings into Lug Stresses Calculator and Equations
    Pressure between a lug and bushing assembly having negative clearance can be determined from consideration of the radial displacements. After assembly, the increase in inner radius of the ring (lug) plus the decrease in outer radius of the bushing equals the difference between the radii of the bushing and ring before assembly.
    Stress at Threaded Tube Connection Design Calculator
    Stress at Threaded Connections Between Two Tubes Design and Calculator
    Hole Sizes Cold Form Tapping Metric Threads
    On materials that can be die cast, cold form tapping can be done in cored holes provided the correct core pin size is used.
    Theoretical Tapping Hole Size Cold Form Threads
    Conventional tap drill sizes should not be used for cold form tapping because the metal is displaced to form the thread.
    Tap Drill Size as Percentage of Engagement Calculator
    The size of the tap drill hole for any desired percentage of full thread depth can be calculated by the formulas below.
    Shock Mach Diamond Formulas and Calculator
    Shock diamonds (also known as Mach diamonds or thrust diamonds) are a formation of standing wave patterns that appear in the supersonic exhaust plume of an aerospace propulsion system
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