A method is proposed for computations of rotordynamic coefficients of deliberately roughened stator gas annular seals using computational fluid dynamics. The method is based on a transient analysis with deforming mesh. Frequency-dependent direct and cross-coupled rotordynamic coefficients are determined as a response to an assigned rotor surface periodic motion. The obtained numerical results are found to be in good agreement with the available test data and one-dimensional tool predictions. The method can be used as a research tool or as a virtual annular seal test rig for seal design and optimization.

1.
Scharrer
,
J.
, 1989, “
Discussion of ‘Annular Honeycomb Seals: Test Results for Leakage and Rotordynamic Coefficients: Comparisons to Labyrinth and Smooth Configurations’
,” by
D.
Childs
,
D.
Elrod
, and
K.
Hale
,
ASME J. Tribol.
0742-4787,
111
, pp.
300
301
.
2.
Yu
,
Z.
, and
Childs
,
D.
, 1998, “
A Comparison of Experimental Rotordynamic Coefficients and Leakage Characteristics Between Hole-Pattern Gas Damper Seals and a Honeycomb Seal
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
120
(
4
), pp.
778
783
.
3.
Moore
,
J.
,
Walker
,
S.
, and
Kuzdzal
,
M.
, 2002, “
Rotordynamic Stability Measurements During Full Load Testing of a 6000psi Re-Injection Centrifugal Compressor
,”
Proc. of 31st Texas A&M University Turbomachinery Symposium
, Turbomachinery Laboratory,
Texas A&M University
,
College Station, TX
, pp.
29
38
.
4.
Moore
,
J. J.
, and
Soulas
,
T. A.
, 2003, “
Damper Seal Comparison in a High-Pressure Re-Injection Centrifugal Compressor During Full-Load, Full-Pressure Factory Testing Using Direct Rotordynamic Stability Measurement
,”
Proc. of ASME Design Engineering Technical Conferences
, Chicago, Sept. 2–6,
ASME
, New York, ASME Paper No. DETC2003/VIB-48458.
5.
Ha
,
T. W.
,
Morrison
,
G.
, and
Childs
,
D.
, 1992, “
Friction-Factor Characteristics for Narrow-Channels With Honeycomb Surfaces
,”
ASME J. Tribol.
0742-4787,
114
, pp.
714
721
.
6.
Chochua
,
G.
,
Shyy
,
W.
, and
Moore
,
J.
, 2002, “
Computational Modeling for Honeycomb-Stator Gas Annular Seal
,”
Int. J. Heat Mass Transfer
0017-9310,
45
, pp.
1849
1863
.
7.
Childs
,
D. W.
,
Shin
,
Y.
, and
Wade
,
J.
, 2006, “
A Design to Increase the Static Stiffness of Hole Pattern Stator Gas Seals
,”
Proc. ASME IGTI Conference
, Barcelona, May 8–11,
ASME
, New York, ASME Paper No. GT2006-90778.
8.
Kleynhans
,
G. F.
, and
Childs
,
D. W.
, 1997, “
The Acoustic Influence of Cell Depth on the Rotordynamic Coefficients of Smooth Rotor/Honeycomb Stator Annular Gas Seals
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
119
, pp.
949
957
.
9.
Moore
,
J. J.
, 2001, “
Three-Dimensional CFD Rotordynamic Analysis of Gas Labyrinth Seals
,”
Proc. of ASME Design Engineering Technical Conferences
, Pittsburgh, Sept. 9–12,
ASME
, New York, ASME Paper No. DETC2001/VIB-21394.
10.
Chochua
,
G.
,
Shyy
,
W.
, and
Moore
,
J.
, 2002, “
Modeling of Compressible Periodic Flows With Application to Turbomachinery Seals
,”
Prog. Comput. Fluid Dyn.
1468-4349,
2
(
1
), pp.
9
19
.
11.
Chochua
,
G.
, and
Shyy
,
W.
, 2003, “
Computational Modeling of Turbulent Flows Over Rough Surfaces
,”
Proc. ASME IMECE Congress & Exposition
, Washington, DC, Nov. 16–21,
ASME
, New York, ASME Paper No. IMECE 2003-41063.
12.
Childs
,
D. W.
, and
Wade
,
J.
, 2004, “
Rotordynamic-Coefficient and Leakage Characteristics for Hole-Pattern-Stator Annular Gas Seals—Measurements versus Predictions
,”
ASME J. Tribol.
0742-4787,
126
, pp.
326
333
.
13.
Childs
,
D. W.
, 1993,
Turbomachinery Rotordynamics: Phenomena, Modeling, and Analysis
,
Wiley
, New York, p.
228
.
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