A new method for predicting the leakage through labyrinth seals has been developed and is shown to provide realistic results which agree with measurements. It utilizes a finite-difference computer code which was developed in order to compute the pressure drop across a single cavity of the seal. This quantity is obtained at several leakage flow Mach numbers to be used subsequently in predicting the leakage rate. The model is widely applicable and does not require an estimate of the kinetic energy carry-over coefficient, whose value is often uncertain for many untested configurations. Detailed cavity distributions of basic flowfield quantities are also presented and examined. Specifically, the predicted results of four seal leakage mass flow rates at given cavity inlet pressure and temperature are compared, and important variations are examined. Also, realistic approximations of flow variable distributions within a single cavity are made from the included figures to assist in the development of analytical methods.
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October 1986
Research Papers
Simulation of Subsonic Flow Through a Generic Labyrinth Seal
D. L. Rhode,
D. L. Rhode
Mechanical Engineering Department, Texas A&M University, College Station, TX 77843
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S. R. Sobolik
S. R. Sobolik
Mechanical Engineering Department, Texas A&M University, College Station, TX 77843
Search for other works by this author on:
D. L. Rhode
Mechanical Engineering Department, Texas A&M University, College Station, TX 77843
S. R. Sobolik
Mechanical Engineering Department, Texas A&M University, College Station, TX 77843
J. Eng. Gas Turbines Power. Oct 1986, 108(4): 674-680 (7 pages)
Published Online: October 1, 1986
Article history
Received:
November 4, 1985
Online:
October 15, 2009
Citation
Rhode, D. L., and Sobolik, S. R. (October 1, 1986). "Simulation of Subsonic Flow Through a Generic Labyrinth Seal." ASME. J. Eng. Gas Turbines Power. October 1986; 108(4): 674–680. https://doi.org/10.1115/1.3239964
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