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0
2
4
6
8
10
0 2 4 6
0
1
2
3
050 100
0
0.2
0.4
0.6
0.8
1
1.2
0500 1000
y = 0.0182x4 - 0.1365x3 + 0.1818x2 + 0.263x + 0.1237
R2 = 1
0.4
0.45
0.5
0.55
0.6
1.5 1.7 1.9 2.1 2.3 2.5 2.7
-1 -0.5 0 0.5 1
-0.4
-0.2
0
0.2
0.4
0.6
0.8
1
-1 -0.5 0 0.5 1
0
0.2
0.4
0.6
0.8
1
-1 -0.5 0 0.5 1
-0.4
-0.2
0
0.2
0.4
0.6
0.8
1
0 2 4 6 8
0
0.5
1not-a-knot
0 2 4 6 8
0
0.5
1clamped
0 2 4 6 8
0
0.5
1pchip
0 2 4 6 8
-0.05
0
0.05 error
0 2 4 6 8
-0.05
0
0.05 error
0 2 4 6 8
-0.2
0
0.2 error
010 20 30 40 50 60 70
0.05
0.1
0.15
0.2
0.25
0.3
0.35
0.4
0.45
0.5
0.55
Re
CD
-2 -1.5 -1 -0.5 0
0
1
2
3
0
2
4
6
8
x1
x2
f(x1,x2)
©
0 5 10 15 20 25 30 35 40
0
200
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600
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1000
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1800 Plot of terminal velocity versus elevation
z (km)
v (m/s)
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