The inclined forces are resolved into vertical and horizontal components in fig.(a)
Now, taking moment about hinged end A
$V_b*4=(86.6*1) + (141.4*2) + (150*3)$
$V_b= 204.85 N and V_a=(86.6+141.4+150)-204.85= 173.15 N$
Resolving Horizontally,
$Ha=50+141.4 + 259.8$
$Ha= 451.20 N$
SF analysis:
SF at any section in $AC = 173.15 N $
SF at any section in $CD= 173.15-86.6=86.55N $
SF at any section in $DE = 150-204.85=-54.85 N $
SF at any section in $EB= - 204.85N. $
BM analysis :
$BM_A = 0$
$BM_B=0$
$BM_C=173.15*1=173.15 Nm $
$BM_D= (173.15*2) - (86.6*1) = 259.7 Nm $
$BM_E= 204.85*1=204.85 Nm$
Thrust analysis: OR Axial face analysis:
Thrust at any section in $AC=451.2N $
Thrust at any Section in $CD=451.2-50=401.2N $
Thrust at any Section in $DE=259.8 N$