Evolution of the flow instabilities in an axial compressor rotor with large tip clearance: An experimental and URANS study
With modern engine designs trending toward smaller cores to increase propulsive efficiency, the gap-to-span ratio in compressors is expected to increase, especially for the rear stages. Detailed knowledge of stronger tip clearance flow and its impact on compressor instability under large clearance c...
Saved in:
| Published in | Aerospace science and technology Vol. 96; p. 105557 |
|---|---|
| Main Authors | , , , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Masson SAS
01.01.2020
|
| Online Access | Get full text |
Cover
Loading…
| Abstract | With modern engine designs trending toward smaller cores to increase propulsive efficiency, the gap-to-span ratio in compressors is expected to increase, especially for the rear stages. Detailed knowledge of stronger tip clearance flow and its impact on compressor instability under large clearance condition become increasingly important. The present study is aiming for illuminating the instability evolution and the underlying flow physics in a large-tip-gap compressor, with the use of casing-mounted pressure transducers to acquire the unsteady nature of tip flow, and full-annulus URANS to obtain the three-dimensional flow details related to instability generation. Results show that flow instability evolution of the compressor along speed-line experiences three stages: stable state, rotating instability, and rotating stall. Two critical behaviors of tip leakage vortex (TLV) are found to relate to the transition of instability pattern. As TLV moves to the adjacent blade trailing edge, it starts to oscillate under the interaction with the adjacent blade, leading to a short-length rotating disturbance, i.e. rotating instability. At near-stall condition, as the interface of TLV and main-flow exceeds the passage inlet plane, forward spillage occurs along with radial vortexes periodically shed from blade leading edge. The periodically generation, movement and decay of leading edge vortexes (LEVs) constitute an orderly propagating disturbance rather than evolve into a stall cell. However, as the compressor is further throttled, the orderly propagation of LEVs collapses due to their scattering, resulting in the generation of stall cells with local stronger blockage and higher entropy. |
|---|---|
| AbstractList | With modern engine designs trending toward smaller cores to increase propulsive efficiency, the gap-to-span ratio in compressors is expected to increase, especially for the rear stages. Detailed knowledge of stronger tip clearance flow and its impact on compressor instability under large clearance condition become increasingly important. The present study is aiming for illuminating the instability evolution and the underlying flow physics in a large-tip-gap compressor, with the use of casing-mounted pressure transducers to acquire the unsteady nature of tip flow, and full-annulus URANS to obtain the three-dimensional flow details related to instability generation. Results show that flow instability evolution of the compressor along speed-line experiences three stages: stable state, rotating instability, and rotating stall. Two critical behaviors of tip leakage vortex (TLV) are found to relate to the transition of instability pattern. As TLV moves to the adjacent blade trailing edge, it starts to oscillate under the interaction with the adjacent blade, leading to a short-length rotating disturbance, i.e. rotating instability. At near-stall condition, as the interface of TLV and main-flow exceeds the passage inlet plane, forward spillage occurs along with radial vortexes periodically shed from blade leading edge. The periodically generation, movement and decay of leading edge vortexes (LEVs) constitute an orderly propagating disturbance rather than evolve into a stall cell. However, as the compressor is further throttled, the orderly propagation of LEVs collapses due to their scattering, resulting in the generation of stall cells with local stronger blockage and higher entropy. |
| ArticleNumber | 105557 |
| Author | Wu, Yadong Deng, Shuanghou Wang, Yangang Wang, Hao |
| Author_xml | – sequence: 1 givenname: Hao surname: Wang fullname: Wang, Hao email: wanghao@nwpu.edu.cn organization: School of Power and Energy, Northwestern Polytechnical University, Xi'an, Shanxi 710072, People's Republic of China – sequence: 2 givenname: Yadong surname: Wu fullname: Wu, Yadong email: yadongwu@sjtu.edu.cn organization: School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai, 200240, People's Republic of China – sequence: 3 givenname: Yangang surname: Wang fullname: Wang, Yangang organization: School of Power and Energy, Northwestern Polytechnical University, Xi'an, Shanxi 710072, People's Republic of China – sequence: 4 givenname: Shuanghou surname: Deng fullname: Deng, Shuanghou organization: School of Power and Energy, Northwestern Polytechnical University, Xi'an, Shanxi 710072, People's Republic of China |
| BookMark | eNp9kNtKAzEQhoNUsK0-gHd5ga1JtnuIXpVSD1AU1F6H2eysTdluliT24NObUq-FYWb-i3_45xuRQWc7JOSWswlnPL_bTMCHiWBcRp1lWXFBhjwXeZIKLgdxFwVLZJ6WV2Tk_YYxJuRUDMnPYmfb72BsR21Dwxpp09o9NZ0PUJnWBIM-KgqxDgZaqu22d-i9ddTZEPvehDVtwX0hDaanukVw0Gm8p7OO4qFHZ7bYhWiFrqar99nrB_Xhuz5ek8sGWo83f3NMVo-Lz_lzsnx7epnPlokWsgiJyJtS5iAlaAGprDQINtVFVuoSMKsbSNMyBV4gQ605L2stcl4I1FNdQVrV6Zjw813trPcOG9XHSOCOijN1gqc2KsJTJ3jqDC96Hs4ejMF2Bp3y2mD8qjYOdVC1Nf-4fwFxUHwK |
| CitedBy_id | crossref_primary_10_1007_s11630_020_1349_4 crossref_primary_10_1016_j_cja_2021_11_001 crossref_primary_10_3390_en14144168 crossref_primary_10_1016_j_ast_2021_106540 crossref_primary_10_1063_5_0156443 crossref_primary_10_1016_j_ast_2022_107459 crossref_primary_10_1063_5_0190152 crossref_primary_10_1016_j_ast_2022_107977 crossref_primary_10_1016_j_ast_2020_106439 crossref_primary_10_1177_09544070211025902 crossref_primary_10_1016_j_ast_2020_106059 crossref_primary_10_1016_j_ast_2022_108070 crossref_primary_10_1016_j_ast_2020_106031 crossref_primary_10_1016_j_ast_2023_108374 crossref_primary_10_1016_j_ast_2024_109100 crossref_primary_10_1115_1_4064085 crossref_primary_10_3390_aerospace11040276 crossref_primary_10_1016_j_ast_2021_107124 crossref_primary_10_1016_j_ast_2021_106752 crossref_primary_10_1016_j_ast_2021_106655 crossref_primary_10_1016_j_ast_2021_106678 crossref_primary_10_3390_en14248369 crossref_primary_10_1016_j_ast_2021_106679 crossref_primary_10_1016_j_ast_2021_107306 crossref_primary_10_33737_jgpps_152718 crossref_primary_10_1016_j_ast_2020_106307 crossref_primary_10_1016_j_ast_2021_106859 crossref_primary_10_1177_09576509211056737 crossref_primary_10_1016_j_ast_2020_106486 crossref_primary_10_1063_5_0090912 |
| Cites_doi | 10.1016/j.ast.2016.09.006 10.1115/1.2841145 10.1115/1.4028686 10.1115/1.2777176 10.1115/1.4025166 10.1016/j.ast.2014.12.004 10.1115/1.1370160 10.1006/jsvi.1996.0890 10.1115/1.3239887 10.1115/1.2718231 10.1016/j.ast.2017.11.012 10.1115/1.2927406 10.1016/j.ast.2018.04.021 10.1016/j.ast.2018.11.058 10.1115/1.1460915 10.1115/1.1303707 10.1115/1.2354522 10.1115/1.4006426 10.1115/1.2841730 10.3390/app7030285 10.1115/1.2929105 |
| ContentType | Journal Article |
| Copyright | 2019 Elsevier Masson SAS |
| Copyright_xml | – notice: 2019 Elsevier Masson SAS |
| DBID | AAYXX CITATION |
| DOI | 10.1016/j.ast.2019.105557 |
| DatabaseName | CrossRef |
| DatabaseTitle | CrossRef |
| DatabaseTitleList | |
| DeliveryMethod | fulltext_linktorsrc |
| Discipline | Engineering |
| EISSN | 1626-3219 |
| ExternalDocumentID | 10_1016_j_ast_2019_105557 S1270963819310995 |
| GroupedDBID | --K --M .~1 0R~ 1B1 1~. 1~5 23M 4.4 457 4G. 5GY 5VS 7-5 71M 8P~ AACTN AAEDT AAEDW AAIAV AAIKJ AAKOC AALRI AAOAW AAQFI AAXUO ABJNI ABMAC ABXDB ABYKQ ACDAQ ACGFS ACNNM ACRLP ADBBV ADEZE ADTZH AEBSH AECPX AEKER AENEX AFKWA AFTJW AGHFR AGUBO AGYEJ AHJVU AHPGS AI. AIEXJ AIKHN AITUG AJBFU AJOXV ALMA_UNASSIGNED_HOLDINGS AMFUW AMRAJ ASPBG AVWKF AXJTR AZFZN BJAXD BKOJK BLXMC CS3 EBS EFJIC EFLBG EJD EO8 EO9 EP2 EP3 FDB FEDTE FGOYB FIRID FNPLU FYGXN G-Q GBLVA HVGLF HZ~ IHE J1W JJJVA KOM M41 MO0 N9A O-L O9- OAUVE OZT P-8 P-9 P2P PC. Q38 R2- RIG ROL RPZ SDF SDG SDP SES SEW SPC SPCBC SST SSZ T5K T9H VH1 XPP ZMT ~G- AAXKI AAYXX AFJKZ AKRWK CITATION |
| ID | FETCH-LOGICAL-c297t-26f896a99ac2a39bca204c758c8ae5dfa3383a17e0ecc118dc26172ec4cba3bd3 |
| IEDL.DBID | .~1 |
| ISSN | 1270-9638 |
| IngestDate | Thu Sep 26 16:21:52 EDT 2024 Fri Feb 23 02:48:30 EST 2024 |
| IsPeerReviewed | true |
| IsScholarly | true |
| Language | English |
| LinkModel | DirectLink |
| MergedId | FETCHMERGED-LOGICAL-c297t-26f896a99ac2a39bca204c758c8ae5dfa3383a17e0ecc118dc26172ec4cba3bd3 |
| ParticipantIDs | crossref_primary_10_1016_j_ast_2019_105557 elsevier_sciencedirect_doi_10_1016_j_ast_2019_105557 |
| PublicationCentury | 2000 |
| PublicationDate | January 2020 2020-01-00 |
| PublicationDateYYYYMMDD | 2020-01-01 |
| PublicationDate_xml | – month: 01 year: 2020 text: January 2020 |
| PublicationDecade | 2020 |
| PublicationTitle | Aerospace science and technology |
| PublicationYear | 2020 |
| Publisher | Elsevier Masson SAS |
| Publisher_xml | – name: Elsevier Masson SAS |
| References | D.C., Shin, Beacher (br0180) 2002 Kameier, Neise (br0260) 1997; 119 McDougall, Cumpsty, Hynes (br0040) 1990; 112 Young, Day, Pullan (br0160) 2011; 135 Wang, Wu, Ouyang (br0280) 2018 Liu, Holste, Neise (br0310) 1996 Camp, Day (br0020) 1998; 120 Pardowitz, Tapken, Neuhaus, Enghardt (br0270) 2015; 137 Weichert, Day (br0060) 2014; 136 Holste, Neise (br0290) 1997; 203 Biela, Muller, Sehiffer (br0110) 2008 Yoon, Song, Shin (br0300) 2006; 128 Liu, Dhingra, Prasad (br0140) 2009 Dhingra, Neumeier, Prasad, Breeze-Stringfellow, Shin, Szucs (br0130) 2006; 129 Garnier, Epstein, Greitzer (br0050) 1991; 113 Moore, Greitzer (br0010) 1986; 108 Inoue, Kuroumaru, Yoshida, Minami, Yamada, Furukawa (br0230) 2004 Wang, Lu, Liu (br0190) 2018; 72 Christensen, Cantin, Gutz, Szucs, Wadia, Armor, Dhingra, Neumeier, Prasad (br0150) 2006; 130 Yamada, Kikuda, Furukawa, Kunjishima, Hara (br0240) 2013 Hoeger, Lahmer, Dupslaff, Fritsch (br0170) 2000; 122 Khaleghi (br0070) 2015; 41 Zhang, Yu, Liu (br0090) 2016; 58 Hah, Voges, Mueller (br0120) 2010 Li, Geng, Du (br0080) 2019; 85 Mailach, Lehmann, Vogeler (br0220) 2001; 123 Day (br0200) 2015 Eck, Geist, Peitsch (br0250) 2017; 7 Righi, Pachidis, Könözsy (br0030) 2018; 78 Bergner, KinLel, Sehiffer (br0100) 2006 März, Hah, Neise (br0210) 2002; 124 Garnier (10.1016/j.ast.2019.105557_br0050) 1991; 113 Zhang (10.1016/j.ast.2019.105557_br0090) 2016; 58 D.C. (10.1016/j.ast.2019.105557_br0180) 2002 Bergner (10.1016/j.ast.2019.105557_br0100) 2006 Liu (10.1016/j.ast.2019.105557_br0140) 2009 Young (10.1016/j.ast.2019.105557_br0160) 2011; 135 Moore (10.1016/j.ast.2019.105557_br0010) 1986; 108 Hoeger (10.1016/j.ast.2019.105557_br0170) 2000; 122 Eck (10.1016/j.ast.2019.105557_br0250) 2017; 7 Pardowitz (10.1016/j.ast.2019.105557_br0270) 2015; 137 Holste (10.1016/j.ast.2019.105557_br0290) 1997; 203 Dhingra (10.1016/j.ast.2019.105557_br0130) 2006; 129 Righi (10.1016/j.ast.2019.105557_br0030) 2018; 78 Christensen (10.1016/j.ast.2019.105557_br0150) 2006; 130 Wang (10.1016/j.ast.2019.105557_br0190) 2018; 72 Li (10.1016/j.ast.2019.105557_br0080) 2019; 85 Liu (10.1016/j.ast.2019.105557_br0310) 1996 Camp (10.1016/j.ast.2019.105557_br0020) 1998; 120 Biela (10.1016/j.ast.2019.105557_br0110) 2008 Yamada (10.1016/j.ast.2019.105557_br0240) 2013 Kameier (10.1016/j.ast.2019.105557_br0260) 1997; 119 Mailach (10.1016/j.ast.2019.105557_br0220) 2001; 123 Wang (10.1016/j.ast.2019.105557_br0280) 2018 Hah (10.1016/j.ast.2019.105557_br0120) 2010 McDougall (10.1016/j.ast.2019.105557_br0040) 1990; 112 Inoue (10.1016/j.ast.2019.105557_br0230) 2004 Yoon (10.1016/j.ast.2019.105557_br0300) 2006; 128 Weichert (10.1016/j.ast.2019.105557_br0060) 2014; 136 Day (10.1016/j.ast.2019.105557_br0200) 2015 März (10.1016/j.ast.2019.105557_br0210) 2002; 124 Khaleghi (10.1016/j.ast.2019.105557_br0070) 2015; 41 |
| References_xml | – year: 2006 ident: br0100 article-title: Short Length-Scale Rotating Stall Inception in a Transonic Axial Compressor: Experimental Investigation contributor: fullname: Sehiffer – year: 2004 ident: br0230 article-title: Effect of Tip Clearance on Stall Evolution Process in a Low-Speed Axial Compressor Stage contributor: fullname: Furukawa – volume: 119 start-page: 460 year: 1997 end-page: 471 ident: br0260 article-title: Experimental study of tip clearance losses and noise in axial turbomachines and their reduction publication-title: J. Turbomach. contributor: fullname: Neise – year: 2009 ident: br0140 article-title: Active Compressor Stability Management via a Stall Margin Control Mode contributor: fullname: Prasad – year: 2013 ident: br0240 article-title: Effects of Tip Clearance on the Stall Inception Process in an Axial Compressor Rotor contributor: fullname: Hara – volume: 112 start-page: 116 year: 1990 end-page: 125 ident: br0040 article-title: Stall inception in axial compressors publication-title: ASME J. Turbomach. contributor: fullname: Hynes – year: 2008 ident: br0110 article-title: Unsteady Pressure Measurement in a Single Stage Axial Transonic Compressor Near the Stability Limit contributor: fullname: Sehiffer – year: 2018 ident: br0280 article-title: Numerical Investigations of Rotating Instability and Unsteady Tip Vortex Structures in an Axial Compressor contributor: fullname: Ouyang – volume: 135 year: 2011 ident: br0160 article-title: Stall warning by blade pressure signature analysis publication-title: ASME J. Turbomach. contributor: fullname: Pullan – volume: 123 start-page: 453 year: 2001 end-page: 463 ident: br0220 article-title: Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex publication-title: ASME J. Turbomach. contributor: fullname: Vogeler – volume: 124 start-page: 367 year: 2002 end-page: 374 ident: br0210 article-title: An experimental and numerical investigation into the mechanisms of rotating instability publication-title: ASME J. Turbomach. contributor: fullname: Neise – volume: 108 start-page: 68 year: 1986 end-page: 76 ident: br0010 article-title: A theory of post-stall transients in axial compression systems: part I – development of equations publication-title: ASME J. Eng. Gas Turbines Power contributor: fullname: Greitzer – volume: 122 start-page: 426 year: 2000 end-page: 432 ident: br0170 article-title: A correlation for tip leakage blockage in compressor blade passages publication-title: ASME J. Turbomach. contributor: fullname: Fritsch – volume: 128 start-page: 1274 year: 2006 end-page: 1280 ident: br0300 article-title: Influence of flow coefficient, stagger angle, and tip clearance on tip vortex in axial compressors publication-title: ASME J. Fluids Eng. contributor: fullname: Shin – year: 2002 ident: br0180 article-title: Effects of loading and clearance variation on tip vortex and endwall blockage publication-title: Ninth International Symposium on Transport Phenomena and Dynamics of Rotating Machinery contributor: fullname: Beacher – volume: 137 year: 2015 ident: br0270 article-title: Experiments on an axial fan stage: time resolved analysis of rotating instability modes publication-title: ASME J. Eng. Gas Turbines Power contributor: fullname: Enghardt – volume: 7 start-page: 285 year: 2017 ident: br0250 article-title: Physics of prestall propagating disturbances in axial compressors and their potential as a stall warning indicator publication-title: Appl. Sci. contributor: fullname: Peitsch – year: 2015 ident: br0200 article-title: Stall, Surge and 75 Years of Research contributor: fullname: Day – volume: 72 start-page: 193 year: 2018 end-page: 203 ident: br0190 article-title: Numerical simulation of unsteady tip clearance flow in a transonic compressor rotor publication-title: Aerosp. Sci. Technol. contributor: fullname: Liu – volume: 136 year: 2014 ident: br0060 article-title: Detailed measurements of spike formation in an axial compressor publication-title: ASME J. Turbomach. contributor: fullname: Day – volume: 78 start-page: 271 year: 2018 end-page: 279 ident: br0030 article-title: Three-dimensional through-flow modelling of axial flow compressor rotating stall and surge publication-title: Aerosp. Sci. Technol. contributor: fullname: Könözsy – volume: 41 start-page: 250 year: 2015 end-page: 258 ident: br0070 article-title: Stall inception and control in a transonic fan, part A: rotating stall inception publication-title: Aerosp. Sci. Technol. contributor: fullname: Khaleghi – volume: 58 start-page: 467 year: 2016 end-page: 479 ident: br0090 article-title: Using wavelets to study spike-type compressor rotating stall inception publication-title: Aerosp. Sci. Technol. contributor: fullname: Liu – year: 2010 ident: br0120 article-title: Characteristics of Clearance Flow Instability in a Transonic Compressor contributor: fullname: Mueller – volume: 129 start-page: 730 year: 2006 end-page: 737 ident: br0130 article-title: A stochastic model for a compressor stability measure publication-title: ASME J. Eng. Gas Turbines Power contributor: fullname: Szucs – volume: 120 start-page: 393 year: 1998 end-page: 401 ident: br0020 article-title: A study of spike and modal stall inception in a low-speed axial compressor publication-title: ASME J. Turbomach. contributor: fullname: Day – volume: 113 start-page: 290 year: 1991 end-page: 302 ident: br0050 article-title: Rotating waves as a stall inception indication in axial compressors publication-title: ASME J. Turbomach. contributor: fullname: Greitzer – year: 1996 ident: br0310 article-title: On the Azimuthal Mode Structure of Rotating Blade Flow Instabilities in Axial Turbomachines contributor: fullname: Neise – volume: 85 start-page: 529 year: 2019 end-page: 543 ident: br0080 article-title: Circumferentially propagating characteristic dominated by unsteady tip leakage flow in axial flow compressors publication-title: Aerosp. Sci. Technol. contributor: fullname: Du – volume: 203 start-page: 641 year: 1997 end-page: 665 ident: br0290 article-title: Noise source identification in a propfan model by means of acoustical near field measurements publication-title: J. Sound Vib. contributor: fullname: Neise – volume: 130 year: 2006 ident: br0150 article-title: Development and demonstration of a stability management system for gas turbine engines publication-title: ASME J. Turbomach. contributor: fullname: Prasad – volume: 58 start-page: 467 year: 2016 ident: 10.1016/j.ast.2019.105557_br0090 article-title: Using wavelets to study spike-type compressor rotating stall inception publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2016.09.006 contributor: fullname: Zhang – year: 2010 ident: 10.1016/j.ast.2019.105557_br0120 contributor: fullname: Hah – year: 2006 ident: 10.1016/j.ast.2019.105557_br0100 contributor: fullname: Bergner – year: 2018 ident: 10.1016/j.ast.2019.105557_br0280 contributor: fullname: Wang – volume: 119 start-page: 460 year: 1997 ident: 10.1016/j.ast.2019.105557_br0260 article-title: Experimental study of tip clearance losses and noise in axial turbomachines and their reduction publication-title: J. Turbomach. doi: 10.1115/1.2841145 contributor: fullname: Kameier – volume: 137 issue: 6 year: 2015 ident: 10.1016/j.ast.2019.105557_br0270 article-title: Experiments on an axial fan stage: time resolved analysis of rotating instability modes publication-title: ASME J. Eng. Gas Turbines Power doi: 10.1115/1.4028686 contributor: fullname: Pardowitz – year: 2002 ident: 10.1016/j.ast.2019.105557_br0180 article-title: Effects of loading and clearance variation on tip vortex and endwall blockage contributor: fullname: D.C. – volume: 130 issue: 3 year: 2006 ident: 10.1016/j.ast.2019.105557_br0150 article-title: Development and demonstration of a stability management system for gas turbine engines publication-title: ASME J. Turbomach. doi: 10.1115/1.2777176 contributor: fullname: Christensen – volume: 136 year: 2014 ident: 10.1016/j.ast.2019.105557_br0060 article-title: Detailed measurements of spike formation in an axial compressor publication-title: ASME J. Turbomach. doi: 10.1115/1.4025166 contributor: fullname: Weichert – year: 2008 ident: 10.1016/j.ast.2019.105557_br0110 contributor: fullname: Biela – year: 2015 ident: 10.1016/j.ast.2019.105557_br0200 contributor: fullname: Day – year: 2009 ident: 10.1016/j.ast.2019.105557_br0140 contributor: fullname: Liu – volume: 41 start-page: 250 year: 2015 ident: 10.1016/j.ast.2019.105557_br0070 article-title: Stall inception and control in a transonic fan, part A: rotating stall inception publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2014.12.004 contributor: fullname: Khaleghi – volume: 123 start-page: 453 issue: 3 year: 2001 ident: 10.1016/j.ast.2019.105557_br0220 article-title: Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex publication-title: ASME J. Turbomach. doi: 10.1115/1.1370160 contributor: fullname: Mailach – volume: 203 start-page: 641 issue: 4 year: 1997 ident: 10.1016/j.ast.2019.105557_br0290 article-title: Noise source identification in a propfan model by means of acoustical near field measurements publication-title: J. Sound Vib. doi: 10.1006/jsvi.1996.0890 contributor: fullname: Holste – volume: 108 start-page: 68 year: 1986 ident: 10.1016/j.ast.2019.105557_br0010 article-title: A theory of post-stall transients in axial compression systems: part I – development of equations publication-title: ASME J. Eng. Gas Turbines Power doi: 10.1115/1.3239887 contributor: fullname: Moore – volume: 129 start-page: 730 issue: 3 year: 2006 ident: 10.1016/j.ast.2019.105557_br0130 article-title: A stochastic model for a compressor stability measure publication-title: ASME J. Eng. Gas Turbines Power doi: 10.1115/1.2718231 contributor: fullname: Dhingra – volume: 72 start-page: 193 year: 2018 ident: 10.1016/j.ast.2019.105557_br0190 article-title: Numerical simulation of unsteady tip clearance flow in a transonic compressor rotor publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2017.11.012 contributor: fullname: Wang – year: 2013 ident: 10.1016/j.ast.2019.105557_br0240 contributor: fullname: Yamada – volume: 112 start-page: 116 issue: 1 year: 1990 ident: 10.1016/j.ast.2019.105557_br0040 article-title: Stall inception in axial compressors publication-title: ASME J. Turbomach. doi: 10.1115/1.2927406 contributor: fullname: McDougall – volume: 78 start-page: 271 year: 2018 ident: 10.1016/j.ast.2019.105557_br0030 article-title: Three-dimensional through-flow modelling of axial flow compressor rotating stall and surge publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2018.04.021 contributor: fullname: Righi – volume: 85 start-page: 529 year: 2019 ident: 10.1016/j.ast.2019.105557_br0080 article-title: Circumferentially propagating characteristic dominated by unsteady tip leakage flow in axial flow compressors publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2018.11.058 contributor: fullname: Li – year: 2004 ident: 10.1016/j.ast.2019.105557_br0230 contributor: fullname: Inoue – volume: 124 start-page: 367 issue: 3 year: 2002 ident: 10.1016/j.ast.2019.105557_br0210 article-title: An experimental and numerical investigation into the mechanisms of rotating instability publication-title: ASME J. Turbomach. doi: 10.1115/1.1460915 contributor: fullname: März – volume: 122 start-page: 426 issue: 2 year: 2000 ident: 10.1016/j.ast.2019.105557_br0170 article-title: A correlation for tip leakage blockage in compressor blade passages publication-title: ASME J. Turbomach. doi: 10.1115/1.1303707 contributor: fullname: Hoeger – volume: 128 start-page: 1274 issue: 6 year: 2006 ident: 10.1016/j.ast.2019.105557_br0300 article-title: Influence of flow coefficient, stagger angle, and tip clearance on tip vortex in axial compressors publication-title: ASME J. Fluids Eng. doi: 10.1115/1.2354522 contributor: fullname: Yoon – volume: 135 issue: 1 year: 2011 ident: 10.1016/j.ast.2019.105557_br0160 article-title: Stall warning by blade pressure signature analysis publication-title: ASME J. Turbomach. doi: 10.1115/1.4006426 contributor: fullname: Young – volume: 120 start-page: 393 year: 1998 ident: 10.1016/j.ast.2019.105557_br0020 article-title: A study of spike and modal stall inception in a low-speed axial compressor publication-title: ASME J. Turbomach. doi: 10.1115/1.2841730 contributor: fullname: Camp – year: 1996 ident: 10.1016/j.ast.2019.105557_br0310 contributor: fullname: Liu – volume: 7 start-page: 285 issue: 3 year: 2017 ident: 10.1016/j.ast.2019.105557_br0250 article-title: Physics of prestall propagating disturbances in axial compressors and their potential as a stall warning indicator publication-title: Appl. Sci. doi: 10.3390/app7030285 contributor: fullname: Eck – volume: 113 start-page: 290 year: 1991 ident: 10.1016/j.ast.2019.105557_br0050 article-title: Rotating waves as a stall inception indication in axial compressors publication-title: ASME J. Turbomach. doi: 10.1115/1.2929105 contributor: fullname: Garnier |
| SSID | ssj0002942 |
| Score | 2.461667 |
| Snippet | With modern engine designs trending toward smaller cores to increase propulsive efficiency, the gap-to-span ratio in compressors is expected to increase,... |
| SourceID | crossref elsevier |
| SourceType | Aggregation Database Publisher |
| StartPage | 105557 |
| Title | Evolution of the flow instabilities in an axial compressor rotor with large tip clearance: An experimental and URANS study |
| URI | https://dx.doi.org/10.1016/j.ast.2019.105557 |
| Volume | 96 |
| hasFullText | 1 |
| inHoldings | 1 |
| isFullTextHit | |
| isPrint | |
| link | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwnV1LS8NAEF6KXvQgPrE-yhw8CbHNZvNYb6W0VMUerIXewmazC5HSlBofePC3O5MmWEEvQi4Ju2GZnZ2Zb_fbGcYurPQEDhDXd6CtIyKfO0kYUT1iGWrpGl-UeQvuR8FwIm6n_rTBevVdGKJVVrZ_ZdNLa119aVfSbC-yrD2mM1NSHwxB6HiHLpoLdH-o01ef3zQPLssCOtTYodb1yWbJ8VLPRKd0JVW79clD_eab1vzNYJftVIEidFdj2WMNM99n22vpAw_YR_-1UhzILWAkB3aWv0FGEV_JeUUUjG-g8HlHPQPijxO8zpewzBFsA-3CwozI4FBkC9BUQ4LU4Bq6c1hP_o__SGHy0B2NoUxIe8gmg_5jb-hUtRQczWVYODywkQyUlEpz5clEK94RGsGCjpTxU6sIqio3NB2cUwQdqaZU7dxooRPlJal3xDbm-dwcM-hYw62K3CAJE2FDLxI6Cq12U4Xhnza8yS5rKcaLVcqMuOaSPcUo8phEHq9E3mSilnP8Y95jNOl_dzv5X7dTtsUJL5dbKGdso1i-mHMMKoqkVWpNi212b-6Goy8jPM1m |
| link.rule.ids | 315,783,787,4509,24128,27936,27937,45597,45691 |
| linkProvider | Elsevier |
| linkToHtml | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwnV07T8MwELZKGYAB8RTleQMTUmjjOA-zVRWoQNuBthJb5Di2VFQ1VSkPMfDbuUsTUSRYkLIksiPrfDl_n_3ljrFzKz2BA8TvO9DWEZHPnSSMqB6xDLV0jS_yvAXdXtAeirtH_7HCWuW_MCSrLGL_Iqbn0bp4Ui-sWZ-ORvU-nZmS-yAEoeMdf4WtCsLH6NSXn986Dy7zCjrU2qHm5dFmLvJSz6SndCWVu_VpifptcVpacG622GaBFKG5GMw2q5jJDttYyh-4yz6uXwvPgcwCQjmw4-wNRgT5ctEr0mC8A4XXOzoakICc-HU2g1mGbBtoGxbGpAaH-WgKmopIkB9cQXMCy9n_8R0pDB-avT7kGWn32PDmetBqO0UxBUdzGc4dHthIBkpKpbnyZKIVbwiNbEFHyvipVcRVlRuaBk4qso5UU652brTQifKS1Ntn1Uk2MQcMGtZwqyI3SMJE2NCLhI5Cq91UIf7ThtfYRWnFeLrImRGXYrKnGE0ek8njhclrTJR2jn9MfIwx_e9uh__rdsbW2oNuJ-7c9u6P2Don8pzvpxyz6nz2Yk4QYcyT09yDvgAd4s7_ |
| openUrl | ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.atitle=Evolution+of+the+flow+instabilities+in+an+axial+compressor+rotor+with+large+tip+clearance%3A+An+experimental+and+URANS+study&rft.jtitle=Aerospace+science+and+technology&rft.au=Wang%2C+Hao&rft.au=Wu%2C+Yadong&rft.au=Wang%2C+Yangang&rft.au=Deng%2C+Shuanghou&rft.date=2020-01-01&rft.pub=Elsevier+Masson+SAS&rft.issn=1270-9638&rft.eissn=1626-3219&rft.volume=96&rft_id=info:doi/10.1016%2Fj.ast.2019.105557&rft.externalDocID=S1270963819310995 |
| thumbnail_l | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1270-9638&client=summon |
| thumbnail_m | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1270-9638&client=summon |
| thumbnail_s | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1270-9638&client=summon |