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`Motivation:
We need data on the best canopy shape for MS16
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Point of max width and height (max frontal area): 900-1100 m from the front of the canopy
15mm fillet radius on the back
CFD conditions:
Minimum Box Values | Maximum Box Values |
---|---|
X min: 0 | X max: 5m |
Y min: 0 | Y max: 4m |
Z min: -15 | Z max: 7.5 |
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Refer to previous canopy shape research for inspirations on your designs.
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Canopy design log:
Version | Pictures | Descriptions/Notes | Sim Results |
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Can 1 (Ryan) | FA = 0.15m^2 Initial/base draft (Ryan) | Cd = 0.0612 Fd = 1.098 | |
Bullet v1 (Gavin) | FA = 0.1458 m^2 Initial Bullet design
| Cd = 0.0701 Fd = 1.222 | |
Can 2 (Ryan) | FA = 0.147m^2 Shrank down front (this was a mistake don’t do that) Shrank down tail on the side profile | Cd = 0.0706 Fd = 1.266 | |
Teardrop v1 | FA = 0.1365 m^2 Base teardrop canopy | Cd = 0.0666 Fd = 1.088 | |
Drop 3 | FA = 0.13 m^2 Shrink down tail side profile to reduce low pressure drag Shrink frontal Area | Cd = 0.066 Fd = 1.036 | |
Drop 4 | FA = 0.136 m^2 experiment with rounding out front side profile to give a more “airfoil”-y shape? definitely worse | Cd = 0.072 Fd = 1.173 | |
Teardrop v3 | FA = 0.166 m^2 Bottom profile made a little straighter, especially near front of canopy | Cd = 0.0668 Fd = 1.328 | |
Teardrop v3.5 | FA = 0.166 m^2 Same canopy as v3, except straightened side profile at the back Performed slightly worse - we can assume that a straight profile will not perform as well (tested in v5.5 - 5.6 as well) | Cd = 0.0669 Fd = 1.330 | |
Teardrop v4 | FA = 0.1478 Flatter side profile , performed much worse than something slightly rounder like v3 | Cd = 0.0735 Fd = 1.300 | |
Teardrop v4.5 | FA = 0.1478 Rounded the side profile and bottom profile out at the front | Cd = 0.0650 Fd = 1.150 | |
Teardrop v5 | FA = 0.1478 Rounded side profile more | Cd = 0.0649 Fd = 1.147 | |
Teardrop v5.5 | FA = 0.1410 Slightly straighter side profile in back half Very low FA | Cd = 0.0639 Fd = 1.078 | |
Teardrop v5.6 | FA = 0.1410 Only change from 5.5 is a very straight back profile, which again did not perform as well | Cd = 0.0667 Fd = 1.126 |
Consider Manufacturability
Keep frontal areas the same- less variation in results
Meeting with interiors for canopy integration
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