Three-Dimensional CST Parameterization Method Applied in Aircraft Aeroelastic Analysis

Table 1

Main parameters of the RLV.

Components	Design parameters	Value
Head-body	Head length	5,000.0 mm
	Body length	11,431.0 mm
	Body width	1,821.0 mm
	Body height upp	1,284.0 mm
	Body height low	405.0 mm
Double wing	Inner wing span length	650.0 mm
	Outer wing span length	2,600.0 mm
	Inner wing root chord length	8,800.0 mm
	Inner wing taper ratio	1.923
	Outer wing taper ratio	2.7
	Inner wing sweep back angle	80.0 deg
	Outer wing sweep back angle	45.0 deg
Tail	Tail span length	1,925.0 mm
	Tail root chord length	2,075.0 mm
	Tail taper ratio	1.724
	Tail sweep back angle	45.0 deg