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J. Influence of friction on the blow-down behavior of anaramid fiber brush seal // ASME Turbo Expo. — Copenhagen,Denmark, 2012. — GT2012-69329.314. Ruggiero E. J., Allen J., Lusted M. Experimental testing techniquesfor Kevlar(r) fiber brush seals // ASME Turbo Expo. — Orlando,FL, USA, 2009. — GT2009-60172.315. San Andrés L., Anderson A.
An all-metal compliant seal versus alabyrinth seal: A comparison of gas leakage at high temperatures //ASME Turbo Expo. — Düsseldorf, Germany, 2014. —GT2014-25572.316. San Andrés L., Ashton Z. Comparison of leakage performance inthree types of gas annular seals operating at a high temperature (300degrees C) // Tribology Transactions. — 2010. — Vol.
53, no. 3. —Pp. 463–471.317. San Andres L., Baker J., Delgado A. Measurements of leakage andpower loss in a hybrid brush seal // Journal of Engineering for GasTurbines and Power. — 2009. — Vol. 131. — P. 012505.443Список литературы318. San Andrés L., Delgado A., Baker J. Rotordynamic force coefficientsof a hybrid brush seal: measurements and predictions // Journal ofEngineering for Gas Turbines and Power. — 2010.
— Vol. 132. —P. 042503.319. Scharrer J. K. Rotordynamic coefficients for stepped labyrinth gasseals // Rotordynamic Instability Problems in High-PerformanceTurbomachinery. — Texas A&M University, USA, 1988. —Pp. 177–195.320. Scharrer J. K. Rotordynamic coefficients for stepped labyrinth gasseals // Journal of Tribology. — 1989.
— Vol. 111. — Pp. 101–107.321. Schmied J. Spiral vibrations of rotors // 11th Biennial ASME DesignEngineering Div. Conf., Vib. Noise, DE-Vol. 2, Rotating MachineryDynamics. — Boston, MA, USA, 1987. — Pp. 449–456.322. Schmied J., Pozivil J., Walch J. Hot spots in turboexpanderbearings: case history, stability analysis, measurements andoperational experience // ASME Turbo Expo. — Berlin, Germany,2008. — GT2008-51179.323. Schwarz H., Friedrichs J. Preliminary investigations for a pressurebalanced back plate at low inclined brush seals // ASME TurboExpo.
— Montreal, Canada, 2015. — GT2015-42580.324. Schwarz H., Friedrichs J., Flegler J. Axial inclination of the bristlepack, a new design parameter of brush seals for improved operationalbehavior in steam turbines // ASME Turbo Expo. — Düsseldorf,Germany, 2014. — GT2014-26330.325. Schwarz H., Friedrichs J., Flegler J. Design parameters of brushseals and their impact on seal performance // ASME TurboExpo. — Copenhagen, Denmark, 2012. — GT2012-68956.326. Sealing in Turbomachinery: tech.
rep. / R. E. Chupp [et al.] ;NASA. — 2006.444Список литературы327. Segmentation effects on brush seal leakage and rotordynamiccoefficients / A. O. Pugachev [et al.] // Journal of Engineering forGas Turbines and Power. — 2016. — Vol. 138, no. 3. —Pp. 032501–9. — DOI: 10.1115/1.4031386.328. Segmented brush seal : US 5176389 / L. E. Noone, L. J. Lagasse. —05.01.1993.329. Sensitivity analysis of squeeze film dampers using Reynoldsequation / A. O. Pugachev [et al.] // 8th IFToMM InternationalConference on Rotor Dynamics.
— Seoul, Korea, 2010. —Pp. 454–462.330. El-Shafei A., Yakoub R. Y. K. Optimum design of squeeze filmdampers supporting multiple-mode rotors // Journal of Engineeringfor Gas Turbines and Power. — 2002. — Vol. 124, no. 4. —Pp. 992–1002.331. Shape optimization of a labyrinth seal applying the simulatedannealing method / V.
Schramm [et al.] // International Journal ofRotating Machinery. — 2004. — Vol. 10, no. 5. — Pp. 365–371.332. Shultz R. R., Vance J. M. Pressure damper diverging labyrinth sealswith circumferential partitions, and method of sealing. — 1996. —US Patent 5,540,447.333. Smirnov P. E., Menter F.
R. Sensitization of the SST turbulencemodels to rotation and curvature by applying the Spalart-Shurcorrection term // ASME Turbo Expo. — Berlin, Germany,2008. — GT2008-50480.334. Soditus S. M. Commerical aircraft maintenance experience relatingto current engine seal technology // 34th AIAA/ASME/SAE/ASEEJoint Propulsion Conference & Exhibit. — Cleveland, OH, USA,1998. — AIAA 98-3284.335. Some metallographic results for brush bristles and brush segments ofa shroud ring brush seal tested in a T 700 engine / R. C. Hendricks[et al.] // Seals Flow Code Development.
— Cleveland, OH, USA,1993. — Pp. 325–366. — N95-13583.445Список литературы336. Some preliminary results of brush seal/rotor interference effects onleakage at zero and low rpm using a tapered rotor / R. Hendricks[et al.] // 27th AIAA/SAE/ASME/ASEE Joint PropulsionConference. — Sacramento, CA, USA, 1991.
— AIAA-91-3390,NASA TM 104396.337. Spalart P. R., Allmaras S. R. A one-equation turbulence model foraerodynamic flows // AIAA 30th Aerospace Sciences Meeting &Exhibit. — Reno, NV, USA, 1992. — AIAA-92-0439.338. Spalart P. R., Shur M. On the sensitization of turbulence models torotation and curvature // Aerospace Science and Technology. —1997. — Vol. 1, no. 5.
— Pp. 297–302. — DOI:10.1016/S1270-9638(97)90051-1.339. Sporer D. R., Reinkensmeier I. High vacuum brazing of Fe-Cr-Al-Yhoneycomb // ASME Turbo Expo. — Vienna, Austria, 2004. —GT2004-53407.340. Stango R. J., Zhao H., Shia C. Y. Analysis of contact mechanics forrotor-bristle interference of brush seal // Journal of Tribology. —2003. — Vol.
125. — Pp. 414–421.341. Stephen D., Hogg S. Development of brush seal technology for steamturbine retrofit applications // ASME International Joint PowerGeneration Conference. — Atlanta, Georgia, USA, 2003. —IJPGC2003-40103.342. Stiffness measurement for pressure-loaded brush seals / R.
A. Bidkar[et al.] // ASME Turbo Expo. — Vancouver, Canada, 2011. —GT2011-45399.343. Stocker H. L., Cox D. M., Holle C. F. Aerodynamic performance ofconventional and advanced design labyrinth seals with solid-smooth,abradable, and honeycomb lands: tech. rep. / Detroit DieselAllison. — 1977. — NASA CR-135307.446Список литературы344. Strauß F., Inagaki M., Starke J.
Reduction of vibration level inrotordynamics by design optimization // Structural andMultidisciplinary Optimization. — 2007. — Vol. 34, issue 2. —Pp. 139–149.345. Structural dynamics optimization of rotor systems for a small-sizeturboprop engine / A. O. Pugachev [et al.] // Journal of Propulsionand Power. — 2015. — Vol. 31, no. 4. — Pp. 1083–1093. — DOI:10.2514/1.B35399.346. Temis J., Selivanov A., Dzeva I. Finger seal design based onfluid-solid interaction model // ASME Turbo Expo. — San Antonio,TX, USA, 2013. — GT2013-95701.347. Temis J., Selivanov A., Dzeva I. Fluid-structural analysis of anon-contacting finger seal // 29th Congress of the InternationalCouncil of the Aeronautical Sciences. — St.
Petersburg, Russia,2014.348. The development of high-performance leaf seals / H. Nakane[et al.] // Journal of Engineering for Gas Turbines and Power. —2004. — Vol. 126. — Pp. 342–350.349. The Tribology Handbook / ed. by M. J. Neale. — 2nd ed. —Butterworth-Heinemann, 1995.350. Theoretical and experimental investigation on tip forces andtemperature distributions of the brush seal coupled aerodynamicforce / S. Huang [et al.] // Journal of Engineering for Gas Turbinesand Power.
— 2014. — Vol. 136. — Pp. 052502–12.351. Thorat M. R., Childs D. W. Predicted rotordynamic behavior of alabyrinth seal as rotor surface speed approaches Mach 1 // Journal ofEngineering for Gas Turbines and Power. — 2010. — Vol. 132. —P. 112504.352. Tisseur F. Backward error and condition of polynomial eigenvalueproblems // Linear Algebra and its Applications. — 2000.
—Vol. 309. — Pp. 339–361.447Список литературы353. Tiwari R., Manikandan S., Dwivedy S. K. A review of theexperimental estimation of the rotor dynamic parameters of seals //The Shock and Vibration Digest. — 2005. — Vol. 37, no. 4. —Pp. 261–284.354. Transient response analysis of large-scale rotor-bearing system withstrong non-linear elements by a transfer matrix-Newmarkformulation integration method / Z.
Gu [et al.] // Journal of Soundand Vibration. — 2003. — Vol. 259. — Pp. 559–570.355. Transient temperature measurements in the contact zone betweenbrush seals of Kevlar and metallic type for bearing chamber sealingusing a pyrometric technique / M. Flouros [et al.] // ASME TurboExpo. — Copenhagen, Denmark, 2012. — GT2012-68354.356. Turner M. T., Chew J. W., Long C.
A. Experimental investigationand mathematical modeling of clearance brush seals // Journal ofEngineering for Gas Turbines and Power. — 1998. — Vol. 120. —Pp. 573–579.357. Tyacke J., Jefferson-Loveday R., Tucker P. On LES methods appliedto seal geometries // ASME Turbo Expo. — Copenhagen, Denmark,2012. — GT2012-68840.358. Unsteady numerical analysis of a whole ring of finger seal withgrooves on finger pads / H. Zhang [et al.] // ASME Turbo Expo.
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