MAE department

MAE 113. Fundamentals of Propulsion (4 units)

Link to catalog page: https://catalog.ucsd.edu/courses/MAE.html#mae113

Description

Compressible flow, thermodynamics, and combustion relevant to aircraft and space vehicle propulsion. Analysis and design of components for gas turbines, including turbines, inlets, combustion chambers and nozzles. Fundamentals of rocket propulsion. Prerequisites: MAE 11 or MAE 110A or CENG 102, and MAE 101A or CENG 101A, and MAE 101B or CENG 101C. Enrollment restricted to MC 25, MC 27, MC 29, MC 30–34, and MC 35–37 majors only.

Prerequisite courses

Successor courses

MAE 113 is a prerequisite of the following 2 courses:

• MAE 114
• MAE 155B