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Stability
T-45A/C TS, E2C2, ADV & IUT Aero-04
D.
Aspect Ratio (AR)
Sg 2, fr 6
Fig 3: Aspect Ratio
1.
Ratio of span of the wing divided by average chord
2.
Fineness ration of the wing that affects aerodynamic
characteristics and structural weight
Figure 3: ASPECT RATIO
E.
Taper
Sg 2, fr 7
Taper
1.
Gradual reduction in chord length from root to tip
2.
Affects lift distribution and structural weight of wing
Page 4-6
(9-99) Original


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