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Shock and Vibration
/
2021
/
Article
/
Fig 9
/
Research Article
Transonic Static Aeroelastic Numerical Analysis of Flexible Complex Configuration Wing
Figure 9
Effects of static aeroelasticity on bomb’s aerodynamic characteristics. (a)
C
L
∼
α
. (b)
C
L
∼
C
D
. (c)
L/D
∼
α
. (d)
C
m
∼
C
L
.
(a)
(b)
(c)
(d)