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Aerodynamic Optimization of the Von Karman Nose Cone for a Supersonic Sounding Rocket

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thesis
posted on 21.05.2021, 09:08 by Taruansh Singh Qaumi
Nose 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 University

Language

eng

Degree

Bachelor of Engineering

Program

Aerospace Engineering

Granting Institution

Ryerson University

LAC Thesis Type

Thesis