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PFR - Aerospace Engineering Sciences Senior Design Projects ...

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Project Final Report – CUDBF April 30 th , 2009<br />

ASEN 4028: <strong>Aerospace</strong> <strong>Senior</strong> <strong>Projects</strong><br />

Figure 46: Streamlines around the Aircraft with the Rockets<br />

The drag estimates for the cases with the payloads on the airplane and the airplane without<br />

payload is summarized in Table 14:<br />

Table 14: Predicted System Drag for Flight Missions from PowerFLOW<br />

Flight Mission Reynolds Number Drag<br />

No Payload on Airplane 708923 1.03 lb<br />

4 Rockets on Airplane 708923 1.43 lb<br />

Bottle on Airplane 708923 1.57 lb<br />

2 Rockets on Airplane 708923 1.30 lb<br />

The analysis was set up to simulate cruise at expected flight conditions in the competition site,<br />

Tucson, Arizona. The maximum drag expected is 1.57 lb which is for the case with the bottle on<br />

the airplane. The results make intuitive sense, since the bottle is not streamlined and therefore<br />

disrupts the flow around it, causing more drag than the rockets.<br />

It is expected that the thrust available is more than required to overcome the predicted drag. This<br />

will be described in the propulsion section. Additionally, this drag prediction will be tested in<br />

flight for comparison purposes. This is detailed in the test and verification section.<br />

75

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