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| AAE 53700 - Hypersonic Propulsion |
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Credit Hours: 3.00. Analysis of advanced high speed air breathing propulsion concepts for hypersonic flight. Missions and trajectories. Engine/airframe integration. Aerothermodynamic analysis of ramjets, scramjets, and oblique detonation wave engines. On- and off-design of compression inlets and minimum length nozzles. Cryogenic fuels and skin cooling. Ram accelerator ballistic launch concepts.
3.000 Credit hours Syllabus Available Levels: Undergraduate, Graduate, Professional Schedule Types: Distance Learning, Lecture Offered By: School of Aero and Astro Engr Department: Aeronautics & Astronautics Course Attributes: Upper Division May be offered at any of the following campuses: West Lafayette Continuing Ed West Lafayette Learning Outcomes: 1. Develop understanding of high-speed inlet systems. 2. Develop understanding of mixing systems employed in airbreathing engines. 3. Develop understanding of turbine-based combined cycle systems. 4. Develop understanding of detonative-based propulsion systems. 5. Develop understanding of ducted rockets. 6. Develop understanding of ramjet and scramjet propulsion systems. Restrictions: May not be enrolled as the following Classifications: Freshman: 15 - 29 hours Sophomore: 45 - 59 hours Freshman: 0 - 14 hours Sophomore: 30 - 44 hours Prerequisites: GR-AAE 53700 Requisites General Requirements: ( Course or Test: AAE 41400 May not be taken concurrently. ) or ( Course or Test: AAE 43900 May not be taken concurrently. ) or ( Student Attribute: GR May not be taken concurrently. ) |
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