Koç, Fatma Serra (2024) How does varying the nozzle diameter of a miniature rocket (2.6 cm, 2.8cm, 3.0cm, 3.2cm,3.4cm,3.6cm, 3.8cm) and the change in the fin angle (30, 40,50) between rocket body and wings affect the maximum altitude that the rocket can reach, and what is the nature of the relationship between nozzle diameter, fin angle and maximum altitude? Other thesis, TED Ankara Koleji.
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Abstract
The study aims to observe how nozzles with (2.6 cm, 2.8cm, 3.0cm, 3.2cm, 3.4cm, 3.6cm, 3.8cm) diameters and the change in fin angle (30°, 40°,50°) affect the maximum height/altitude and try to find the nature of the relationship between nozzle diameter, fin angle and maximum altitude by using the Newton`s Laws of Motion. This experiment also focuses on the development of rockets and contributes to the implications of fields of rocket science under the topic “mechanics”.
| Item Type: | Thesis (Other) |
|---|---|
| Uncontrolled Keywords: | Mechanics, nozzle diameter |
| Subjects: | Q Science > QC Physics |
| Depositing User: | Kamil Çömlekçi |
| Date Deposited: | 08 Oct 2024 12:03 |
| Last Modified: | 08 Oct 2024 12:03 |
| URI: | http://tedprints.tedankara.k12.tr/id/eprint/1306 |
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