This paper describes an innovative, three-day, turbomachinery research project for Japanese and British high-school students. The project is structured using modern teaching theories that encourage student curiosity and creativity. The experience develops teamwork and communication and helps to break down the cultural and linguistic barriers between students from different countries and backgrounds. The approach provides a framework for other hands-on research projects that aim to inspire young students to undertake a career in engineering. The project is part of the Clifton Scientific Trust's annual UK–Japan Young Scientist Workshop Programme. This work focuses on compressor design for jet engines and gas turbines. It includes lectures introducing students to turbomachinery concepts, a computational design study of a compressor blade section, experimental tests with a low-speed cascade, and tutorials in data analysis and aerodynamic theory. The project also makes use of 3D printing technology, so that students go through the full engineering design process, from theory, through design, to practical experimental testing. Alongside the academic aims, students learn what it is like to study engineering at university, discover how to work effectively in a multinational team, and experience a real engineering problem. Despite a lack of background in fluid dynamics and the limited time available, the lab work and end-of-project presentation show how far young students can be stretched when they are motivated by an interesting problem.
Skip Nav Destination
Article navigation
Research-Article
A Computational and Experimental Compressor Design Project for Japanese and British High-School Students
S. D. Grimshaw,
S. D. Grimshaw
Whittle Laboratory,
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
e-mail: sdg33@cam.ac.uk
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
e-mail: sdg33@cam.ac.uk
Search for other works by this author on:
C. L. Sequeira,
C. L. Sequeira
Whittle Laboratory,
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
Search for other works by this author on:
M. Hewkin-Smith
M. Hewkin-Smith
Whittle Laboratory,
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
Search for other works by this author on:
S. D. Grimshaw
Whittle Laboratory,
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
e-mail: sdg33@cam.ac.uk
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
e-mail: sdg33@cam.ac.uk
C. L. Sequeira
Whittle Laboratory,
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
M. Hewkin-Smith
Whittle Laboratory,
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
University of Cambridge,
1 JJ Thomson Avenue,
Cambridge CB3 0DY, UK
1Present address: Hybrid Air Vehicles Ltd, Hangar 1, Cardington Airfield, Shortstown, Bedford MK42 0TG, UK.
Contributed by the Education Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received August 22, 2016; final manuscript received September 14, 2016; published online January 10, 2017. Editor: David Wisler.
J. Eng. Gas Turbines Power. May 2017, 139(5): 052604 (9 pages)
Published Online: January 10, 2017
Article history
Received:
August 22, 2016
Revised:
September 14, 2016
Citation
Grimshaw, S. D., Sequeira, C. L., and Hewkin-Smith, M. (January 10, 2017). "A Computational and Experimental Compressor Design Project for Japanese and British High-School Students." ASME. J. Eng. Gas Turbines Power. May 2017; 139(5): 052604. https://doi.org/10.1115/1.4035208
Download citation file:
Get Email Alerts
Cited By
Temperature Dependence of Aerated Turbine Lubricating Oil Degradation from a Lab-Scale Test Rig
J. Eng. Gas Turbines Power
Multi-Disciplinary Surrogate-Based Optimization of a Compressor Rotor Blade Considering Ice Impact
J. Eng. Gas Turbines Power
Experimental Investigations on Carbon Segmented Seals With Smooth and Pocketed Pads
J. Eng. Gas Turbines Power
Related Articles
Undergraduate Project in Compressor Rig Design, Fabrication, and Testing for Complete Engineering Training
J. Eng. Gas Turbines Power (May,2016)
Thermodynamics and Fluid Mechanics of a Closed Blade Cascade Wind Tunnel for Organic Vapors
J. Eng. Gas Turbines Power (May,2016)
Investigations on the Effects of Inflow Condition and Tip Clearance Size to the Performance of a Compressor Rotor
J. Eng. Gas Turbines Power (December,2014)
Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions
J. Eng. Gas Turbines Power (December,2015)
Related Proceedings Papers
Related Chapters
Boundary Layer Analysis
Centrifugal Compressors: A Strategy for Aerodynamic Design and Analysis
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Introduction
Turbine Aerodynamics: Axial-Flow and Radial-Flow Turbine Design and Analysis