An Experimental and Numerical Investigation of the Rotordynamic Coefficients of a Gas Labyrinth Seal: Part 2 - Numerical Simulation

Abstract Part 1 of this paper presented the experimental investigation of the rotordynamic behavior of a six-tooth gas labyrinth seal. In part 2, the rotordynamic force coefficients and leakage flow of the labyrinth seal were predicted using a bulk-flow model (BFM) and a computational fluid dynamics (CFD) model. The CFD model solved the Reynolds-averaged Navier-Stokes (RANS) equations with a Spalart-Allmaras turbulence model. A grid independence study was conducted in both the meridional plane and circumferential direction using four different node configurations for both studies. A grid that offered a good compromise between computational cost and solution accuracy was determined. The quasi-steady state method was employed using combinations of four different subsynchronous precessional frequency ratios (PFR) to find the rotordynamic coefficients. Additionally, the shaft was statically displaced 5, 10, and 20 percent of the radial clearance and it was found that the solution did not vary with displacement. A 10 percent displacement was chosen to conduct the rest of the numerical simulations. The comparison between the experimental and computational results showed a good agreement for the rotordynamic coefficients that did not vary with frequency. However, when frequency dependence behavior was observed, the direct damping coefficient was underpredicted by both the bulk-flow model and CFD. Furthermore, the leakage was overpredicted by the numerical results. Because the direct damping coefficient was underpredicted and the leakage was overpredicted, the numerical results were considered conservative. It was also found that refining the mesh improved the agreement between experimental and CFD results, underscoring the importance of mesh choice in accurately modeling the seal’s behavior. Finally, the CFD prediction outperformed the bulk-flow model, but the computational cost of the CFD simulations far exceeded that of the bulk-flow model.

Authors

Institutions

Publication Details

Published
2025-06-16
DOI
https://doi.org/10.1115/gt2025-153994
Primary Topic
Tribology and Lubrication Engineering
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

An Experimental and Numerical Investigation of the Rotordynamic Coefficients of a Gas Labyrinth Seal: Part 2 - Numerical Simulation

Paul G. A. Cizmas, Ciprian R. Comsa
Tribology and Lubrication Engineering
article

An Experimental and Numerical Investigation of the Rotordynamic Coefficients of a Gas Labyrinth Seal: Part 2 - Numerical Simulation

Paul G. A. Cizmas, Ciprian R. Comsa
article en

Abstract

Abstract Part 1 of this paper presented the experimental investigation of the rotordynamic behavior of a six-tooth gas labyrinth seal. In part 2, the rotordynamic force coefficients and leakage flow of the labyrinth seal were predicted using a bulk-flow model (BFM) and a computational fluid dynamics (CFD) model. The CFD model solved the Reynolds-averaged Navier-Stokes (RANS) equations with a Spalart-Allmaras turbulence model. A grid independence study was conducted in both the meridional plane and circumferential direction using four different node configurations for both studies. A grid that offered a good compromise between computational cost and solution accuracy was determined. The quasi-steady state method was employed using combinations of four different subsynchronous precessional frequency ratios (PFR) to find the rotordynamic coefficients. Additionally, the shaft was statically displaced 5, 10, and 20 percent of the radial clearance and it was found that the solution did not vary with displacement. A 10 percent displacement was chosen to conduct the rest of the numerical simulations. The comparison between the experimental and computational results showed a good agreement for the rotordynamic coefficients that did not vary with frequency. However, when frequency dependence behavior was observed, the direct damping coefficient was underpredicted by both the bulk-flow model and CFD. Furthermore, the leakage was overpredicted by the numerical results. Because the direct damping coefficient was underpredicted and the leakage was overpredicted, the numerical results were considered conservative. It was also found that refining the mesh improved the agreement between experimental and CFD results, underscoring the importance of mesh choice in accurately modeling the seal’s behavior. Finally, the CFD prediction outperformed the bulk-flow model, but the computational cost of the CFD simulations far exceeded that of the bulk-flow model.

Texas A&M University (US)
Openalex Percentile: Top 80%
Tribology and Lubrication Engineering
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.

An Experimental and Numerical Investigation of the Rotordynamic Coefficients of a Gas Labyrinth Seal: Part 2 - Numerical Simulation — Paul G. A. Cizmas, Ciprian R. Comsa · (2025) | TGRS Research Map | TGRS