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

Table 4

Wing tip displacements when , semispan.

q (Pa)	LE				TE
	VLM + linear	VLM + nonlinear	Experiment	CFD/CSD	VLM + linear	VLM + nonlinear	Experiment	CFD/CSD
117	2.13	2.13	2.57	2.51	1.78	1.78	1.90	2.11
153	3.22	3.22	3.42	3.88	2.70	2.70	2.92	3.25
194	4.97	4.96	5.44	6.16	4.16	4.16	4.50	5.17
216	6.27	6.23	6.77	7.90	5.25	5.22	5.69	6.62
239	8.06	7.92	9.62	10.33	6.75	6.64	8.25	8.66
251	9.24	9.01	11.57	12.01	7.73	7.54	9.76	10.07
264	10.78	10.37	15.05	15.72	9.03	8.69	12.71	13.19
276	12.55	11.85	18.69	16.75	10.51	9.92	15.81	14.07
289	14.98	13.71	21.75	21.25	12.54	11.49	18.62	17.89
310	20.74	17.42		28.81	17.37	14.60		24.30
324	26.91	20.42		32.50	22.52	17.12		27.42
338	36.98	23.84		35.47	30.96	19.99		29.93
352	56.44	27.62		38.29	47.24	23.17		32.34
367	117.30	31.89		41.51	98.18	26.77		35.07