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Shock and Vibration
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2018
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Article
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Tab 1
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Research Article
Aerodynamics Optimization of a Ducted Coaxial Rotor in Forward Flight Using Orthogonal Test Design
Table 1
Forward flight aerodynamics factor-level form.
Factor level
Pitch angle (
/°)
Flight velocity (
/m·s
−1
)
Rotor spacing (H/mm)
1
A
1
85
B
1
5
C
1
38
2
A
2
80
B
2
10
C
2
57
3
A
3
75
B
3
15
C
3
66.5
4
A
4
70
B
4
20
C
4
76