Computational Methods in Aerospace Engineering

A simulation of flow over a cylinder.

Mach 2 inviscid flow simulation over a cylinder, from Project #1. (Image courtesy of Professor Darmofal.)

Instructor(s)

MIT Course Number

16.901

As Taught In

Spring 2005

Level

Undergraduate

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Course Features

Course Description

This course serves as an introduction to computational techniques arising in aerospace engineering. Applications are drawn from aerospace structures, aerodynamics, dynamics and control, and aerospace systems. Techniques include: numerical integration of systems of ordinary differential equations; finite-difference, finite-volume, and finite-element discretization of partial differential equations; numerical linear algebra; eigenvalue problems; and optimization with constraints.

Darmofal, David. 16.901 Computational Methods in Aerospace Engineering, Spring 2005. (MIT OpenCourseWare: Massachusetts Institute of Technology), http://ocw.mit.edu/courses/aeronautics-and-astronautics/16-901-computational-methods-in-aerospace-engineering-spring-2005 (Accessed). License: Creative Commons BY-NC-SA


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