The effect of bullet aerodynamics modeled after Falco peregrinus and Istiophorus on drag force
2015
- 93Usage
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Example: if you select the 1-year option for an article published in 2019 and a metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019. If you select the 3-year option for the same article published in 2019 and the metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019, 2018 and 2017.
Citation Benchmarking is provided by Scopus and SciVal and is different from the metrics context provided by PlumX Metrics.
Metrics Details
- Usage93
- Abstract Views93
Artifact Description
Bullets have been used in warfare and in sports for many years, and one of the limits is the distance the bullets can travel. Different aerodynamic characteristics from some of the fastest animals are implemented into bullet designs for this study, to look for an increase in speed or distance. A control .223 bullet design template was used to create two modified bullets, the first modified bullet had the front half of Istiophorus (sailfish), and the back half of Falco Peregrinus (peregrine falcon), and the second modified bullet had the front half of Falco Peregrinus and the back half of Istiophorus. The designs were printed using a 3D printer, and a Paxton-Patterson wind tunnel was used to find the amount of drag force exerted on the bullet. It was hypothesized that at least one of the modified bullets would be more aerodynamic than the control bullet. A one-way ANOVA test (F(2,87)= 25486.53, p <0.001) rejected the null hypothesis that there was no significant difference. Tukey tests were performed and it was found that there were significant differences between all 3 of the bullet shapes. This means that modified bullet 2 is the most aerodynamic of the bullets, and both of the bullets are more aerodynamic than the traditional bullet.
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