A simply supported beam of constant flexural rigidity and length 2 L carries a concentrated load 'P' at its mid-span and the deflection under that load is \[\delta .\] if a cantilever beam of the same flexural rigidity length is subjected to load ?P? at its free end, them the deflection at the free end will be:

• A. \[1/2\delta \]                  
• B. \[\delta \]
• C. \[2\delta \]                                 
• D. \[4\delta \]