Experimental and Numerical Studies on Static Aeroelastic Behaviours of a Forward-Swept Wing Model

Table 3

Wing tip displacements when , semispan.

q (Pa)	LE				TE
	VLM + linear	VLM + nonlinear	Experiment	CFD/CSD	VLM + linear	VLM + nonlinear	Experiment	CFD/CSD
152	2.12	2.13	2.11	2.59	1.78	1.78	1.85	2.17
192	3.25	3.25	3.56	4.08	2.72	2.72	3.04	3.42
238	5.31	5.29	5.64	7.00	4.45	4.43	4.85	5.86
262	7.01	6.92	8.08	9.57	5.87	5.80	6.67	8.02
275	8.26	8.07	9.43	11.48	6.91	6.76	8.09	9.63
287	9.71	9.34	12.40	13.78	8.13	7.83	10.42	11.56
310	13.83	12.58	17.09	21.65	11.57	10.53	14.57	18.22
324	17.93	15.16		28.55	15.01	12.71		24.07
338	24.65	18.32		33.09	20.63	15.36		27.92
352	37.62	22.02		36.40	31.49	18.46		30.73
367	78.19	26.47		40.00	65.44	22.21		33.78