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Shock Tube 1

2024

Abstract

Shock tubes provide a more affordable method of producing and studying shock waves than supersonic wind tunnels. A shock wave is a phenomenon which occurs when a wave passes through a fluid faster than the speed of sound in that fluid. This project explored the design, manufacturing, and testing of a shock tube that can be used in an undergraduate lab environment at the University of South Carolina. This system should be able to record important shock wave parameters such as pressures, temperatures, and wave speed. Creating and visualizing this phenomenon can be helpful in helping students understand it better. This shock tube is designed based on requirements and constraints following the needs of the aerospace engineering program. The technical aspects of the design process involved various considerations including computational fluid dynamics (CFD) simulation, Finite Element Analysis, structural design, and more.

Project Details

The requirements were to create a safe shock tube which could generate supersonic shockwaves. This had to be under 4m (compact), able to be moved, and include a way to visualize shockwaves and collect data.

Project Objective 

Design a shock tube to create and analyze compressible flow phenomena in a lab setting with 5 people within 3 months and within budget requirements

Mission Needs

Produce shockwaves within a control volume and measure parameters such as pressure and velocity.

Media Gallery

Team Poster

Project Report

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