Beam Bending with End Overhanging Supports and a Single Load

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Design Variables
Modulus of Elasticity (E) =
Moment of Inertia (I) =
Load (W) =
Distance (c) =
Distance (d) =
Distance (w) =
Distance (u) =
Distance (l) =
Distance (x) =
Distance to nuetral axis/plane =
Results
Load at support [(W(c + l)]/l  =
Load at support -(Wc)/l =
Stress between nearest support  (s) =
Stress between the two supports (s) =
Stress at the support nearest the load (s) =
Deflection between load nearest (adjacent support) (y) =
Deflection between supports ( y) =
Defelction between non-loaded end and nearest support (y) =
Deflection at the load (y) =
Deflection at the unloaded ends (y) =
Section Modulus (Z) =