Author

Andrew Girgis

Date of Award

2025

Document Type

Thesis

Degree Name

Master of Science (MS)

Department

Aerospace Systems Engineering

Committee Chair

Philip Ligrani

Committee Member

Haiyang Hu

Committee Member

Jason Cassibry

Research Advisor

Philip Ligrani

Subject(s)

Particle image velocimetry, Shock waves, Aerodynamics

Abstract

Presented is the development of a Particle Image Velocimetry (PIV) apparatus to quantify the velocity field produced by an oblique shock wave and its reflections in a supersonic/transonic wind tunnel. A flow seeding system is developed using mesquite wood smoke generated in a metal vessel heated with a Vevor TDGC-2KVA variable autotransformer. A pressurized K-bottle drives the smoke through a cooled copper coil and moisture trap to remove contaminants before injection. A dual-pulsed class IV Nd:YAG Big Sky laser with Thorlabs optomechanical components, including two cylindrical lenses, is used to create a pulsed light sheet to illuminate tracer particles. Image pairs are captured using a Phantom V711 camera synchronized using a LaserPulse 610036 synchronizer. PIV measurements are processed in PIVlab software to calculate the velocity field. Measured velocity distributions provide evidence of a turbulent shear layer and a recirculation zone in the vicinity of the oblique shock wave reflection.

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