Airfoil Surface Forming and Conformity Test Using Laser Tracker

Table 3

Tracker reading taken on top of molding board at different points.

Point group
S plate top 48 points
Point name	X	Y	Z
P1	−976.2759	−2140.5612	−481.2692
P2	−980.7335	−2152.6343	−481.1536
P3	−990.3482	−2161.4971	−481.0501
P4	−1002.4197	−2166.3966	−480.97
P5	1015.3528	−2168.9338	−480.9115
P6	−1028.0954	−2169.1193	−480.8853
P7	1039.5915	−2175.751	−480.7797
P8	1051.2279	−2180.9598	−480.6912
P9	−1062.93	−2186.9736	−480.5963
P10	−1074.0302	−2193.5324	−480.5214
P11	−1086.9986	−2194.064	−480.4546
P12	−1100.1986	−2193.6767	−480.4198
P13	−1113.294	−2192.2552	−480.3864
P14	−1125.9616	−2188.2754	−480.3779
P15	−1136.6008	−2180.2742	−480.4053
P16	−1146.6413	−2171.8494	−480.4606
P17	−1157.5336	−2164.7377	−480.4818
P18	−1168.7838	−2158.7666	−480.4981
P19	−1179.8543	−2150.9762	−480.5279
P20	−1187.1016	−2140.3997	−480.5796
P21	−1193.4046	−2129.0944	−480.6606
P22	−1199.829	−2118.0557	−480.7184
P23	−1207.6435	−2107.6629	−480.79
P24	−1221.0255	−2104.9024	−480.7788
P25	−1234.5046	−2104.706	−480.7413
P26	−1247.5803	−2104.92	−480.6895
P27	−1260.3825	−2105.782	−480.6336
P28	−1273.1835	−2107.0054	−480.5874
P29	−1284.4976	−2113.5615	−480.4824
P30	−1295.991	−2119.1133	−480.3963
P31	−1307.4492	−2125.1469	−480.3033
P32	−1318.0271	−2132.5771	−480.2127
P33	−1328.8502	−2139.4026	−480.1214
P34	−1341.2087	−2143.6695	−480.0521
P35	−1353.1007	−2137.2685	−480.0626
P36	−1364.4663	−2128.7971	−480.0957
P37	−1375.1794	−2121.4027	−480.127
P38	−1388.0924	−2117.9434	−480.1141
P39	−1400.971	−2113.3679	−480.1125
P40	−1413.037	−2108.683	−480.1131
P41	−1424.4997	−2101.7101	−480.1446
P42	−1435.7663	−2095.6768	−480.1587
P43	−1447.0337	−2089.7746	−480.17
P44	−1446.5152	−2102.7926	−480.0616
P45	−1448.6624	−2116.0266	−479.9442
P46	−1451.685	−2129.1464	−479.8188
P47	−1455.0269	−2141.7487	−479.706
P48	−1461.8059	−2152.6271	−479.5961
S plate 48-point fit plane
Flatness		Measured
RMS		0.0386
		0.0079