Remote laboratory exercises are gaining popularity due to advances in communication technologies along with the need to provide realistic yet flexible educational tools for tomorrow’s engineers. Laboratory exercises in turbomachinery aerodynamics generally involve substantial equipment in both size and power, so the development of remotely controlled facilities has perhaps not occurred as quickly as in other fields. This paper presents an overview of a new interactive laboratory exercise involving aerodynamics in a linear cascade of stator blades. The laboratory facility consists of a high-speed fan that delivers a maximum of 2.5 kg/s of air to the cascade. Traversing pneumatic probes are used to determine pressure profiles at upstream and downstream locations, and loss coefficients are later computed. Newly added equipment includes cameras, stepper motors, and a data acquisition and control system for remote operation. This paper presents the laboratory facility in more detail and includes discussions related to user interface issues, the development of a virtual laboratory exercise as a complement to experiments, and comparative evaluation of Virtual, Remote and Local laboratory exercises.
Skip Nav Destination
ASME Turbo Expo 2004: Power for Land, Sea, and Air
June 14–17, 2004
Vienna, Austria
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
0-7918-4166-9
PROCEEDINGS PAPER
Web-Based, Interactive Laboratory Experiment in Turbomachine Aerodynamics
Nalin Navarathna,
Nalin Navarathna
Royal Institute of Technology, Stockholm, Sweden
Search for other works by this author on:
Vitalij Fedulov,
Vitalij Fedulov
Royal Institute of Technology, Stockholm, Sweden
Search for other works by this author on:
Andrew Martin,
Andrew Martin
Royal Institute of Technology, Stockholm, Sweden
Search for other works by this author on:
Torsten Fransson
Torsten Fransson
Royal Institute of Technology, Stockholm, Sweden
Search for other works by this author on:
Nalin Navarathna
Royal Institute of Technology, Stockholm, Sweden
Vitalij Fedulov
Royal Institute of Technology, Stockholm, Sweden
Andrew Martin
Royal Institute of Technology, Stockholm, Sweden
Torsten Fransson
Royal Institute of Technology, Stockholm, Sweden
Paper No:
GT2004-54032, pp. 885-891; 7 pages
Published Online:
November 24, 2008
Citation
Navarathna, N, Fedulov, V, Martin, A, & Fransson, T. "Web-Based, Interactive Laboratory Experiment in Turbomachine Aerodynamics." Proceedings of the ASME Turbo Expo 2004: Power for Land, Sea, and Air. Volume 1: Turbo Expo 2004. Vienna, Austria. June 14–17, 2004. pp. 885-891. ASME. https://doi.org/10.1115/GT2004-54032
Download citation file:
11
Views
Related Proceedings Papers
Related Articles
Web-Based, Interactive Laboratory Experiment in Turbomachine Aerodynamics
J. Turbomach (January,2010)
Three-Component LDV Measurements in the Wake of a Compressor Cascade With Flow Separation
J. Turbomach (January,2008)
Related Chapters
Alternative Systems
Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII: Theory, History and Practice—Guidance from the Past for Modern Engineers and Students
QP Based Encoder Feedback Control
Robot Manipulator Redundancy Resolution
Other Components and Variations
Axial-Flow Compressors