MAE 5510

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MAE 5510

Course information provided by the Courses of Study 2023-2024.

Introduction to air and rocket propulsion. Emphasis on air-breathing gas-turbines. Chemical rocket propulsion. Brief discussion of of ramjets and of propellers. Application of thermodynamic and fluid-mechanical principles to analysis of performance and design, including fuel efficiency and environmental impacts.

When Offered Spring.

Prerequisites/Corequisites Prerequisite: ENGRD 2210/MAE 2210 and MAE 3230 or equivalents. Recommended prerequisite: MAE 3050.

Outcomes
  • Students will be able to describe and interpret the types, characteristics, and performance measures of combustion engines used in propulsion, power generation, and road vehicles.
  • Students will be able to apply thermodynamic and fluid mechanical principles to quantitatively describe engine operation.
  • Students will be able to predict how their performance depends on design parameters and operating conditions.

View Enrollment Information

Syllabi: none
  •   Regular Academic Session.  Choose one lecture and one project. Combined with: MAE 4510

  • 4 Credits Graded

  •  9433 MAE 5510   LEC 001

    • WF Olin Hall 165
    • Jan 22 - May 7, 2024
    • Fisher, E

    • M Olin Hall 245
    • Jan 22 - May 7, 2024
    • Fisher, E

  • 19668 MAE 5510   PRJ 601

  • As part of this graduate section, the student must complete 40 hours of asynchronous project work for this additional credit.

Syllabi: none
  •   Regular Academic Session.  Choose one lecture and one project.

  • 4 Credits Graded

  • 19666 MAE 5510   LEC 002

  • Instruction Mode: Distance Learning-Asynchronous

  • 19667 MAE 5510   PRJ 602

    • TBA
    • Jan 22 - May 7, 2024
    • Fisher, E

  • Instruction Mode: Distance Learning-Asynchronous
    As part of this graduate section, the student must complete 40 hours of asynchronous project work for this additional credit.