The University of Texas Rio Grande Valley

MECE 4315 Propulsion

This course provides an introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers. The course is divided into four parts: basic concepts and gas dynamics; analysis of rocket propulsion systems; parametric (design point) and performance (off-design) analysis of air breathing propulsion systems; and analysis and design of major gas turbine engine components (fans, compressors, turbines, inlets, nozzles, main burners, and afterburners). Design concepts are introduced early and integrated throughout.

Credits

3

Prerequisite

A grade of 'C' or better in MECE 3315.

Schedule Type

Lecture

Grading Basis

Standard Letter (A-F)

Administrative Unit

Mechanical Engineering

Offered

Fall/Spring/Summer