College

College of Engineering (COE)

Date of Last Revision

2020-05-07 11:31:23

Major

Mechanical Engineering - Cooperative Education

Honors Course

4600:497

Number of Credits

4

Degree Name

Bachelor of Science

Date of Expected Graduation

Spring 2020

Abstract

Air entering the engine of a supersonic aircraft must be slowed to subsonic speeds for the engine to perform properly and not become significantly damaged over time. Diffusers are designed to create a shockwave to slow down air to subsonic speeds before the air enters the engine. This project will focus on the numerical analysis and design of diffuser geometries for supersonic aircraft engines. The main objective is to evaluate supersonic flow over different geometries, specifically the interaction between shock waves and boundary layer, and to minimize the amount of drag created by different diffuser geometries to optimize the efficiency of the diffuser.

Research Sponsor

Alex Povistky

First Reader

Nicholas Garafolo

Second Reader

Scott Sawyer

Honors Faculty Advisor

Donald Quinn

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