$\backslash$table$[[$Length of compressor,$110$ mm$],[$Length of combustor,$350$ mm$],[$Length of turbine,$60$ mm$],[$Total length,$520$ mm$]]$

$1$

mm

Loads

Reactions

Figure $5\mathrm{.}2$: Load diagram of the shaft.

Figure $5\mathrm{.}4$: Moment diagram of the shaft.

Table $5\mathrm{.}1$: Specifications of the turbo jet engine.

$\backslash$table$[[$Hub radius of the turbine,$0\mathrm{.}0487$ m$],[$Hub radius of the compressor,$0\mathrm{.}015$ m$],[$Thrust $($Axial Force$),618\mathrm{.}452$ N$],[$gross weight,$768\mathrm{.}26$ kg$],[$Angular speed,$5728\mathrm{.}2ra\frac{d}{s}$