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April 1986
Technical Briefs
Effects of Tip Endwall Contouring on the Three-Dimensional Flow Field in an Annular Turbine Nozzle Guide Vane: Part 2—Numerical Investigation
T. Arts
T. Arts
von Karman Institute for Fluid Dynamics, B-1640 Rhode Saint Gene`se, Belgium
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T. Arts
von Karman Institute for Fluid Dynamics, B-1640 Rhode Saint Gene`se, Belgium
J. Eng. Gas Turbines Power. Apr 1986, 108(2): 426-428 (3 pages)
Published Online: April 1, 1986
Article history
Received:
May 29, 1985
Online:
October 15, 2009
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A commentary has been published:
Discussion: “Theory Versus Experiment for the Rotordynamic Coefficients of Annular Gas Seals: Part 1—Test Facility and Apparatus” (Childs, D. W., Nelson, C. E., Nicks, C., Scharrer, J., Elrod, D., and Hale, K., 1986, 108, pp. 426–431)
A companion article has been published:
Theory Versus Experiment for the Rotordynamic Coefficients of Annular Gas Seals: Part 2—Constant-Clearance and Convergent-Tapered Geometry
Citation
Arts, T. (April 1, 1986). "Effects of Tip Endwall Contouring on the Three-Dimensional Flow Field in an Annular Turbine Nozzle Guide Vane: Part 2—Numerical Investigation." ASME. J. Eng. Gas Turbines Power. April 1986; 108(2): 426–428. https://doi.org/10.1115/1.3239922
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