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Micro-Jet Test Facility for Aerospace Propulsion Engineering Education

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Abstract:

This paper describes the methodology that has been developed and implemented at the School of Aeronautics (ETSIA) of the Universidad Politecnica de Madrid (UPM) to familiarize aerospace engineering students with the operation of real complex jet engine systems. This methodology has a two-pronged approach: students carry out preparatory work by using, first, a gas turbine performance prediction numerical code; then they validate their assumptions and results on an experimental test rig. When looking at the educational aspects, we have taken care that, apart from being sufficiently robust and flexible, the experimental set-up is similar to real jet engine rigs, so the students are not constrained to exploring a much too limited parametric space. Also, because a facility like this is usually subject to extensive and somewhat rugged use, we have focused on a low cost design.

Keywords: AEROSPACE PROPULSION; MICRO-JET ENGINE TEST FACILITY

Document Type: Research Article

Publication date: January 1, 2009

More about this publication?
  • This journal serves as an international interdisciplinary forum of reference for engineering education.
    A balance between papers on developments in educational methods technology, case studies, laboratory applications, new theoretical approaches, educational policy and survey papers is aimed for.
    Comprehensive coverage of new education schemes and techniques makes the journal a unique source of ideas for engineering educators who are keen to keep abreast of latest developments in educational applications in all fields of engineering.
    Some of the areas covered more extensively in recent issues are: CAD, CAE, computer applications in teaching thermodynamics, material science, electrical engineering, new courses and curricula, engineering management, control engineering, mechanical engineering, engineering design, student evaluation and institutional accreditation.
intjee/ijee/2009/00000025/00000001/art00003
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