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References

1
Huber, F. W., Johnson, P. D., Sharma, O. P., Staubach, J. B., and Gaddis, S. W., "Performance Improvement Through Indexing of Turbine Airfoils: Part I - Experimental Investigation,'' ASME Paper 95-GT-27, Houston, TX, 1995, also to appear in the ASME Journal of Turbomachinery.

2
Griffin, L. W., Huber, F. W., and Sharma, O. P., "Performance Improvement Through Indexing of Turbine Airfoils: Part II - Numerical Simulation,'' ASME Paper 95-GT-28, Houston, TX, 1995, also to appear in the ASME Journal of Turbomachinery.

3
Dorney, D. J., Sharma, O. P., "A Study of Turbine Performance Increases Through Airfoil Clocking," AIAA Paper 96-2816, Lake Buena Vista, FL, 1996.

4
Gundy-Burlet, K. L., and Dorney, D. J., "Physics of Airfoil Clocking in Axial Compressors,'' accepted for presentation at the 1997 ASME Gas Turbine Conference and Exposition, to be held June 2-5, 1997, Orlando, FL.

5
Gundy-Burlet, K. L., "Computations of Unsteady Multistage Compressor Flows in a Workstation Environment," ASME Paper 91-GT-336, Orlando, FL, 1991.

6
Rai, M. M., "Navier-Stokes Simulations of Rotor/Stator Interactions Using Patched and Overlaid Grids," AIAA Journal of Propulsion and Power, Vol. 3, No. 5, Sept., 1987, pp.387-396.

7
Rai, M. M., Madavan, N. K. and Gavali, S., "Multipassage Navier-Stokes Simulations of Turbine Rotor-Stator Interaction," AIAA Journal of Propulsion and Power, Vol. 9, No. 3, May-June, 1993, pp. 389-396.

8
B. S. Baldwin and H. Lomax, "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flow," AIAA Paper 78-257, Huntsville, AL, January, 1978.

9
Gundy-Burlet, K. L., Rai, M. M., and Dring, R. P., "Two-Dimensional Computations of Multistage Compressor Flows Using a Zonal Approach," AIAA Paper 89-2452, Monterey, CA, July, 1989.

10
AGARD, "Test Cases for Computation of Internal Flows in Aero Engine Components," AGARD Propulsion and Energetics Panel, Working Group 18, AGARD-AR-275, 1989.

11
Gundy-Burlet, K. L., Rai, M. M., Stauter, R. C., and Dring, R. P., "Temporally and Spatially Resolved Flow in a Two-Stage Axial Compressor, Part 2 - Computational Assessment," J. Turbomachinery, Vol. 113, No. 2, April, 1991, pp. 227-232.

12
Oates, G. C., , AIAA Educational Series, 1984.


Karen L. Gundy-Burlet
Fri Jul 25 15:51:15 PDT 1997