Aeroelastic Optimization Design for High-Aspect-Ratio Wings with Large Deformation

Table 3

Lumped mass.

Leading edge		Trailing edge
Number	(kg)	Number	(kg)
1	0.1427	1	0.1168
2	0.1282	2	0.1110
3	0.1292	3	0.1012
4	0.1076	4	0.0834
5	0.0861	5	0.0675
6	0.0744	6	0.0569
7	0.0435	7	0.0440
8	0.0349	8	0.0354
9	0.0258	9	0.0261
10	0.0254	10	0.0256
11	0.0177	11	0.0178