ASE 376K - Propulsion

Institution:

The University of Texas at Austin

Subject:

Description:

Review of control volume analysis and quasi-one-dimensional compressible flow. Analysis and design of rocket nozzles and airbreathing engines, including performance and cycle analysis; the flow in nozzles, diffusers, compressors, and turbines; and combustion chamber processes and propellants. Includes an introduction to chemical and electric rocket propulsion. Three lecture hours a week for one semester. Prerequisite: Aerospace Engineering 362K with a grade of at least C-.

Credits:

3.00

Credit Hours:

Prerequisites:

Corequisites:

Exclusions:

Level:

Instructional Type:

Lecture

Notes:

Additional Information:

Historical Version(s):

Institution Website:

www.utexas.edu

Phone Number:

(512) 471-3434

Regional Accreditation:

Southern Association of Colleges and Schools

Calendar System:

Semester

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