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TECHNICAL PAPERS

Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk

[+] Author and Article Information
A. J. Sanders, K. K. Hassan

Honeywell Engines, Systems & Services, 111 South 34th Street, MS 301-134, Phoenix, AZ 85034

D. C. Rabe

Air Force Research Laboratory, 1950 Fifth Street, Building 18D, Wright Patterson AFB, OHe-mail: Douglas.Rabe@afrl.af.mil

J. Turbomach 126(1), 166-174 (Mar 26, 2004) (9 pages) doi:10.1115/1.1645532 History: Received December 01, 2002; Revised March 01, 2003; Online March 26, 2004
Copyright © 2004 by ASME
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References

Jeffers,  J. D., and Meece,  C. E., 1975, “F100 Stall Flutter Problem Review and Solution,” AIAA J. Aircr., 12(4), pp. 350–359.
El-Aini, Y. M., Bankhead, H. R. and Meece, C. E., 1986, “Subsonic/Transonic Stall Flutter Investigation of an Advanced Low Pressure Compressor,” ASME Paper No. 86-GT-90.
El-Aini, Y. M., and Capece, V. M., 1995, “Stall Flutter Prediction Techniques for Fan and Compressor Blades,” AIAA Paper No. 95-2652.
Adamcyzk,  J. J., Stevans,  W., and Jutras,  R., 1982, “Supersonic Stall Flutter of High-Speed Fans,” ASME J. Eng. Power, 104(3), pp. 675–682.
Shibata, T., and Kaji S., 1998, “Role of Shock Structures in Transonic Fan Rotor Flutter,” Proceedings of the 8th International Symposium of Unsteady Aerodynamics and Aeroelasticity of Turbnomachines, Kluwer, Dordrecht, The Netherlands, pp. 733–747.
Isomura,  K., and Giles,  M. B., 1998, “A Numerical Study of Flutter in a Transonic Fan,” ASME J. Turbomach., 120, pp. 500–507.
Silkowski, P. D., Rhie, C. M., Copeland, G. S., Eley, J. A., and Bleeg, J. M., 2001, “CFD Investigation of Aeromechanics,” ASME Paper No. 2001-GT-0267.
Srivastava, R., Bakhle, M. A., Keith Jr., T. G., and Stefko, G. L., 2002, “Flutter Analysis of a Transonic Fan,” ASME Paper No. GT-2002-30319.
Carta,  F. O., and St. Hilaire,  A. O., 1978, “Experimentally Determined Stability Parameters of a Subsonic Cascade Oscillating Near Stall,” ASME J. Eng. Power, 100, pp. 111–120.
Carta,  F. O., and St. Hilaire,  A. O., 1980, “Effect of Interblade Phase Angle and Incidence Angle on Cascade Pitching Stability,” ASME J. Eng. Power, 102, pp. 391–396.
Carta,  F. O., 1983, “Unsteady Aerodynamics and Gapwise Periodicity of Oscillating Cascaded Airfoils,” ASME J. Eng. Gas Turbines Power, 105, pp. 565–574.
Buffum, D. H., Capece, V. R., King, A. J., and El-Aini, Y. M., 1996, “Experimental Investigation of Unsteady Flows at Large Incidence Angles in a Linear Oscillating Cascade,” AIAA Paper No. 96-2823.
Buffum, D. H., Capece, V. R., King, A. J., and El-Aini, Y. M., 1996, “Oscillating Cascade Aerodynamics at Large Mean Incidence,” ASME Paper No. 96-GT-339.
Hardin, L. W., Carta, F. O., and Verdon, J. M., 1987, “Unsteady Aerodynamic Measurements on a Rotating Blade Row at Low Mach Number,” ASME Paper No. 87-GT-221.
Frey, K. K., and Fleeter, S., 1996, “Oscillating Airfoil Aerodynamics of a Rotating Compressor Blade Row,” AIAA Paper No. 96-2673.
Stargardter, H., 1979, “Subsonic/Transonic Stall Flutter Study,” NASA CR-165256.
Halliwell,  D. G., Newton,  S. G., and Lit,  K. S., 1984, “A Study of Unsteady Pressures Near the Tip of a Transonic Fan in Unstalled Supersonic Flutter,” ASME J. Vib., Acoust., Stress, Reliab. Des., 106, pp. 198–203.
Shabbir, A., and Zhu, J., 1996, “Assessment of Three Turbulence Models in a Compressor Rotor,” ASME Paper No. 96-GT-198.
Bakhle, M. A., Srivastava, R., and Keith Jr., T. G., 1997, “A 3D Euler/Navier-Stokes Aeroelastic Code for Propulsion Applications,” AIAA Paper No. 97-2749.
Bakhle, M. A., Srivastava, R., and Keith Jr., T. G., 1998, “Aeroelastic Calculations Based on Three-Dimensional Euler Analysis,” AIAA Paper No. 98-3295.
Chen, J. P., and Whitfield, D. L., 1993, “Navier-Stokes Calculations for the Unsteady Flowfield of Turbomachinery,” AIAA Paper No. 93-0676.
Srivastava, R., Bakhle, M. A., and Keith Jr., T. G., 1999, “Phase-Lagged Boundary Condition Methods for Aeroelastic Analysis of Turbomachines—A Comparative Study,” ASME Paper No. 99-GT-19.
Adamczyk,  J. J., Celestina,  M. L., and Greitzer,  E. M., 1993, “The Role of Tip Clearance in High-Speed Fan Stall,” ASME J. Turbomach., 115, pp. 28–38.
Chima,  R. V., 1998, “Calculation of Tip Clearance Effects in a Transonic Compressor Rotor,” ASME J. Turbomach., 120, pp. 131–140.
Van Zante, D. E., Strazisar, A. J., Wood, J. R., Hathaway, M. D., and Okiishi, T. H., 1999, “Recommendations for Achieving Accurate Numerical Simulation of Tip Clearance Flows in Transonic Compressor Rotors,” ASME Paper No. 99-GT-390.
Feiner, D. M., and Griffin, J. H., 2003, “Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part 1: Theory,” ASME Paper No. GT2003-38952.
Feiner, D. M., and Griffin, J. H., 2003, “Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part 2: Application,” ASME Paper No. GT2003-38953.

Figures

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Phase-lock averaged suction surface waveforms
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Steady 90% span blade-to-blade Mach number
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Aerodynamic damping versus nodal diameter
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Effect of tip clearance on flutter boundary predictions
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Effect of tip clearance on loading predictions
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Effects of vibration amplitude on flutter boundary predictions
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Effects of vibration amplitude on loading predictions
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CFD grid for unsteady TURBO-AE simulations
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Mode shape for unsteady TURBO-AE simulations
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Flush-mounted Kulites at 90% span
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Fan map with flutter test and analysis points
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Phase-lock averaged pressure surface waveforms
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Effect of number of time steps-per-cycle on flutter boundary predictions
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Effect of number of time steps-per-cycle on loading predictions

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