Holography has been developed by Rolls-Royce as a technique for routine use in the evaluation of fan designs for aeroengines. It is used to investigate both aerodynamic and mechanical behavior of the rotating fan. Holographic flow visualization provides clear, three-dimensional images of the transonic flow region between the fan blades. Flow features such as shocks, shock/boundary layer interaction, and over-tip leakage vortices can be observed and measured. Holograms taken through an optical derotator allow vibration modes of the rotating fan to be mapped during resonance or flutter. Examples are given of the use of both techniques at rotational speeds up to and in excess of 10,000 rpm. Holography has provided valuable information used to verify and improve numerical modeling of the fan behavior and has been successful in evaluating the achievement of design intent.
Skip Nav Destination
Article navigation
July 1988
Research Papers
The Use of Holographic Interferometry for Turbomachinery Fan Evaluation During Rotating Tests
R. J. Parker,
R. J. Parker
Advanced Research Laboratory, Rolls-Royce plc, Derby, United Kingdom
Search for other works by this author on:
D. G. Jones
D. G. Jones
Advanced Research Laboratory, Rolls-Royce plc, Derby, United Kingdom
Search for other works by this author on:
R. J. Parker
Advanced Research Laboratory, Rolls-Royce plc, Derby, United Kingdom
D. G. Jones
Advanced Research Laboratory, Rolls-Royce plc, Derby, United Kingdom
J. Turbomach. Jul 1988, 110(3): 393-400 (8 pages)
Published Online: July 1, 1988
Article history
Received:
February 19, 1987
Online:
November 9, 2009
Citation
Parker, R. J., and Jones, D. G. (July 1, 1988). "The Use of Holographic Interferometry for Turbomachinery Fan Evaluation During Rotating Tests." ASME. J. Turbomach. July 1988; 110(3): 393–400. https://doi.org/10.1115/1.3262209
Download citation file:
Get Email Alerts
Cited By
Related Articles
Influence of Deposit on the Flow in a Turbine Cascade
J. Turbomach (October,1988)
Study of Wake-Blade Interactions in a Transonic Compressor Using Flow Visualization and DPIV
J. Fluids Eng (March,2002)
Computation of the Unsteady Transonic Flow in Harmonically Oscillating Turbine Cascades Taking Into Account Viscous Effects
J. Turbomach (January,1998)
Interferometric Measurements in a Turbine Cascade Using Image-Plane Holography
J. Eng. Power (January,1981)
Related Chapters
Aerodynamic Performance Analysis
Axial-Flow Compressors
Vortex-Induced Vibration
Flow Induced Vibration of Power and Process Plant Components: A Practical Workbook
Numerical Simulations of Tip Leakage Vortex Cavitation Flows Around a NACA0009 Hydrofoil
Proceedings of the 10th International Symposium on Cavitation (CAV2018)