ugg stivali Compressor casing circumferential groo

Compressor casing treatment circumferential grooves of the axial position

The aerodynamic load distribution characteristics of film determined. Reference: Eli Lu new roots, CHU Wu-li. Axial Compressor Casing Treatment Research and Review EJ]. Advances in Mechanics, 2006,36 (2) :222-223. [2] WILKEI. ANumericalinvestigationoftheflowmechanismsinahighpressurecompressorfrontstagewithaxi-alslots [J]. JournalofTurbomachinery,[link widoczny dla zalogowanych], 2004,126 (3) :333-349. [3] HOFMANW,[link widoczny dla zalogowanych], BALLMANNJ. Tipclearancevortexdevelopmentandshock-vortex-interactioninatransonicaxialcompressorrotor [R]. AIAAPaperNo2002-0083. rSl_], 2002. [43 Lu new roots, CHU Wu-li, Zhang Yanfeng. Transonic compressor casing clearance flow and processing analysis of interaction [J]. Xi'an Jiaotong University, 2006,40 (11) :1357-1360. LUXinggen, CHUWuli. ZHANGYanfengoNumericalinvestigationofinteractionbetweencasingtreatmentandtipleakageflowinatransoniccompressorrotor [J]. JournalofXi'anJiaoTongUniversity, 2006,40 (11) :1357-1360. [5] Jiang Li,[link widoczny dla zalogowanych], obliterate. Rotor tip clearance with the inter-tone multi-block grid simulation and design of compressor [D]. Beijing: Beijing University of Aeronautics. 2004. LIMi ~ iang. Numericalinvestigationanddesignoftran ~ soniccompressorswithtipclearanceflowusingmulti ~ blockmesh [D]. Beijing: 13eijingUniversityofAeronau ~ ticsandAstronautics, 2004. [6] Wang Yongming, Wu Chun, Tu Baofeng, et al. With the fan casing treatment transonic unsteady numerical simulation [J]. Nanjing University of Aeronautics and Astronautics, 2006,[link widoczny dla zalogowanych],38 (5) :540-544. . WANGYongrning, HUJun, TUBaofeng, eta1. Un ~ steadynumericalsimulationoftransonicfanwithcasingtreatment [J]. JournalofNanjingUniversityofAero-nauticsandAstronautics, 2006,38 (5) :540-544. [7] DUNHAMJ. CFDvalidationforpropulsionsystemcom ~ ponent [R]. AGARDAR-355. IS. 1. ], 1998. [8] BAILYEE. Effectsofgroovedcasingtreatmentontheflowrangecapabilityofasinglestageaxial - floweompres - sor [R]. NASATMX-2459. IS. 1_], 1972. [9] Lau. Circumferential groove casing treatment on the number of observations [J]. Northwestern Polytechnical University, 1985,3 (2) :207-217. r1O] FURUKAWAM,[link widoczny dla zalogowanych], INOUEM, SAIKIK, YAMADAK. Theroleoftipleakagevortexbreakdownincom-pressorrotoraerodynamics [R]. AsMEPaperNo. 98 a GT_239. IS. 1_], 1998.

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