A Study of a Reconnaissance Surveillance Vehicle
A Study of a Reconnaissance Surveillance Vehicle
A Study of a Reconnaissance Surveillance Vehicle
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Wing Lift Coefficient<br />
1.40<br />
1.20<br />
1.00<br />
0.80<br />
0.60<br />
0.40<br />
0.20<br />
0.00<br />
-0.20<br />
-0.40<br />
Drag Polar<br />
Drag Polar at Mach=0.60<br />
(AEDC-16T TF-910), Mach=0.60, RN/mac= 0.877x10^6<br />
0.00 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08<br />
Drag Coefficient<br />
NPS041003 39
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