Abstract
A shear and stress sensitive film (S3F) is employed on the suction surface of an industry standard low-pressure turbine blade. These tests address the optimization of S3F for low-speed air investigations on a curved surface, and are the first measurements of its kind. S3F provides all three stress components on a surface in a single measurement, and is based on 3D elastic deformations of a polymeric film. A detailed description of the S3F technique is presented along with proof of concept experiments, followed by the turbine results which illustrate the need for separate films tailored for the local stress levels in each area. Oil–film verification of stresses is also included.
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Abbreviations
- c :
-
chord length
- C f :
-
skin friction coefficient
- dC p :
-
change in pressure coefficient, \({\rm d}C_{\rm p}=\frac{{\rm d}P}{0.5\,mU^2}\)
- G :
-
Green’s functions of influence
- h :
-
film thickness
- m :
-
density of air
- Re :
-
Reynold's number, \(Re=\frac{Uc}{\nu}\)
- S :
-
contact surface
- u :
-
displacement fields
- U :
-
characteristic velocity
- η :
-
dynamic viscosity of oil
- ε :
-
deformation tensor
- λ :
-
Lame constant, \(\lambda=\frac{2\mu \nu}{1-2\nu}\)
- μ :
-
shear modulus of elasticity
- ν :
-
Poisson ratio
- ρ :
-
S3F density
- τ :
-
shear stress
- θ :
-
volume deformation
- x :
-
streamwise direction
- y :
-
surface-normal direction
- z :
-
cross-stream direction
References
Bell H, Schairer E, Hand L, Mehta R (2001) Surface pressure measurements using luminescent coating. Ann Rev Fluid Mech 33:155–206
Black M, Anadan P (1993) Framework for robust estimation of optical flow. In: Presented at 4th international conference on computer vision (ICCV93)
Bons J, Hansen L, Clark J, Koch P, Sondergaard R (2005) Designing low-pressure turbine blades with integrated flow control. ASME Paper No. GT2005-68962
Braess D (2002) Finite elements, 2nd edn. Cambridge University Press, London
Crafton J, Fonov S, Jones G, Fonov V (2005) Optical measurements of pressure and shear in a plasma. In: AIAA paper no. AIAA-2005-5006
Curtis E, Hodson H, Banieghbal M, Denton J, Howell R, Harvey N (1997) Development of blade profiles for low-pressure turbine applications. J Turbo 119:531–538
Danaila I, Hecht F, Pironneau O (2003) Simulation numerique en C++. Dunod, Paris, France
Denton J (1993) Loss mechanisms in turbomachines. J Turbo 115(4):621–656
Fonov V (2002) Development and analysis of data processing methods applied to luminescent coating system in aerodynamics. PhD thesis, Herriot–Watt University, England
Fonov S, Goss L, Jones G, Crafton J, Fonov V, Ol M (2005) New method for surface pressure measurements. AIAA paper no. AIAA-2005-1029
Hakkinen R (2004) Reflections on fifty years of skin friction measurement. AIAA paper no. AIAA-2004-2111
Howell R, Ramesh O, Hodson H, Harvey N, Schulte V (2001) High lift and aft-loaded profiles for low-pressure turbines. J Turbo 123:181–188
Kobayashi T (2002) Handbook of particle image velocimetry. Morikita Chuppan
Liu T, Sullivan J (1998) Luminescent oil–film skin-friction meter. AIAA J 36(8)
Liu T, Sullivan J (2005) Pressure and temperature sensitive paints. Springer, Berlin
Mayle R (1991) The role of laminar-turbulent transition in gas turbine engines. J Turbo 113:509–537
Plesniak M, Peterson S (2004) Wall shear stress measurements for conventional applications and biomedical flows (invited). (AIAA paper no. AIAA-2004-2301)
Praisner T, Clark J (2004) Predicting Transition in Turbomachinery. Part I: A review and new model development. ASME paper no. IGTI-2004-54108
Sharma O, Pickett G, Ni R (1990) Assessment of unsteady flows in turbines. ASME paper no. 90-GT-150
Soemarwoto B, Boelens O (2003) Simulation of vortical flow over a slender delta wing experiencing vortex breakdown. NLR-TP-2003-396:27
Tarasov V, Orlov A (1990) Method for determining shear stress on aerodynamic model surface. Patent of Russia, 4841553/23/1990
Tobak M, Peake D (1982) Topology of three-dimensional separated flows. Ann Rev Fluid Mech 14:61–85
Tyler C, Fonov S, Goss L, Crafton J, Jones E, Sarka B (2004) Comparison of computationally predicted and experimentally measured skin friction. AIAA paper no. AIAA-2004-2304
Acknowledgments
The first author wishes to thank the Dayton Area Graduate Studies Institute for financial support. All authors would like to thank Andrew Lethander and Chris Murphy of AFRL for their assistance with the rapid prototyping of the LPT blade, and Grant Jones of ISSI for assistance with the S3F formulation.
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McQuilling, M., Wolff, M., Fonov, S. et al. An experimental investigation of a low-pressure turbine blade suction surface using a shear and stress sensitive film. Exp Fluids 44, 73–88 (2008). https://doi.org/10.1007/s00348-007-0375-2
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DOI: https://doi.org/10.1007/s00348-007-0375-2