AE 598

Spring 2013 All Classes

All Classes

Credit: 1 TO 4 hours.

Subject offerings of new and developing areas of knowledge in aerospace engineering intended to augment existing formal courses. Topics and prerequisites vary for each section. See Class Schedule or departmental course information for both.

May be repeated in the same or separate terms if topics vary to a maximum of 12 hours.

Section Status updates every 10 minutes.
AE 598 class schedule data for spring 2013
CRN Type Section Time Day Location Instructor Section Details
49926
Lecture-Discussion
CAA
10:30AM -12:20PM
TR
104 Talbot Laboratory
Bodony, D
Part of Term:
1
Date Range:
01/14/13-05/01/13
Credit:
4 hours
Section Info:
4 hours Topic: Aeroacoustics. Physical mechanisms and mathematical modeling of sound generation and flow-sound interaction; An overview of aeroacoustics theories and computational approaches; Advanced turbulence simulation techniques (DNS, LES, unsteady RANS) for evaluation nonlinear sound sources; Accurate numerical methods and boundary conditions for direct computation of sound generation and propagation. Both engineering biological systems (e.g., the human voice) will be discussed. Prerequisites: Intermediate level courses in fluid mechanics and CFD (or numerical methods).
59630
Online
EL
ARRANGED
n.a.
n.a.
Loth, E
Part of Term:
1
Date Range:
01/14/13-05/01/13
Credit:
4 hours
Section Title:
Comp. Methods Multiphase Flow
Section Info:
4 credit hours The course focuses on the methodologies for multiphase simulation starting with categorizing common numerical approaches for multiphase flow. This includes guidelines for choosing "tools" (numerical approaches) for a particular ?job? (particle and flow conditions) based on ?performance? (predictive ability) and ?cost? (computational requirements). The rest of the course will then consider specific numerical techniques for: very small particles that are in equilibrium or near-equilibrium with the surrounding fluid, moderate-size particles that have significant relative velocity and treated with point-force approaches and very large particles treated with resolved-surface methods for whereby the flowfield around the surface is discretized and directly simulated.
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