Qaumi_Taruansh_Singh.pdf (2.7 MB)
Aerodynamic Optimization of the Von Karman Nose Cone for a Supersonic Sounding Rocket
thesis
posted on 2021-05-21, 09:08 authored by Taruansh Singh QaumiNose cone design is very much reliant on the conditions of the rocket’s flight path. The design is dependant on the altitude, velocity profile, materials, and other factors. This report will look at optimizing a rocket nose cone design based on preliminary measurements, aerodynamic factors, and engineering design process. This analysis will be done utilizing ANSYS Fluent to conduct CFD on 2D symmetric Von Karman nose cones of varying fineness ratios.
History
Editor
Ryerson UniversityLanguage
engDegree
- Bachelor of Engineering
Program
- Aerospace Engineering
Granting Institution
Ryerson UniversityLAC Thesis Type
- Thesis Project