Airfoil Surface Forming and Conformity Test Using Laser Tracker

Table 4

Tracker reading taken on the edge of molding board.

Point group
Template movement1
Point name	X	Y	Z
P3	−913.8005	−2249.0049	−379.9377
P4	−926.466	−2247.0901	−379.8765
P5	−939.199	−2245.1128	−379.8617
P6	−951.938	−2243.1981	−379.8542
P7	−964.6058	−2241.1748	−379.822
P8	−977.3165	−2239.2531	−379.7737
P9	−989.937	−2237.3306	−379.7452
P10	−1002.5128	−2235.4107	−379.7243
P11	−1015.1814	−2233.4538	−379.6771
P12	−1027.916	−2231.491	−379.6557
P13	−1040.549	−2229.4971	−379.6318
P14	−1053.4084	−2227.3414	−379.62
P15	−1066.1477	−2225.359	−379.5878
P16	−1079.0193	−2223.4518	−379.571
P17	−1091.8151	−2221.4101	−379.5435
P18	−1104.4108	−2219.4773	−379.5111
P19	−1117.0033	−2217.5725	−379.4726
P20	−1129.634	−2215.6122	−379.4237
P21	−1142.2915	−2213.6537	−379.3974
P22	−1154.8561	−2211.6965	−379.3587
P23	−1167.4701	−2209.7026	−379.3317
P24	−1180.2329	−2207.6841	−379.3061
P25	−1192.8917	−2205.8501	−379.2798
P26	−1205.7916	−2203.8835	−379.283
P27	−1218.6228	−2201.8677	−379.2645
P28	−1231.2455	−2199.9227	−379.2504
P29	−1244.1254	−2197.9692	−379.2212
P30	−1256.8553	−2195.9994	−379.1809
P31	−1269.7158	−2194.0569	−379.1668
P32	−1282.3553	−2192.0388	−379.1503
P33	−1295.1198	−2190.0632	−379.114
P34	−1307.7332	−2188.1677	−379.0868
P35	−1320.3828	−2186.3373	−379.0773
P36	−1332.9954	−2184.4885	−379.05
P37	−1345.8163	−2182.4824	−379.0345
Template1 fit line
Linearity		Measured
RAM		0.2179
		0.0918