Web Optimization of Compression Ignition Aviation Engine Crankshaft

Table 6

Analysis results.

Iteration	Δ mass [%]	Δ stress [%]
Reference	0	0
#0 (Manual)	-18.8	+34.2
#1	-17.9	+26.1
#2	-16.4	+28.7
#3	-18.0	+24.2
#4	-15.6	+16.3
#5	-15.2	+20.5
#6	-17.2	+15.7
#7	-14.1	+10.8
#8	-17.6	+17.0
#9	-16.1	+11.9
#10	-16.8	+14.4