Gust response of rigid and elastically mounted airfoils at a transitional Reynolds number
This article explores the evolution of the unsteady flow structure for rigid and elastically mounted NACA0012 airfoils subject to a parallel vortical gust disturbance at a Reynolds number of Re=150,000 using implicit large-eddy simulation coupled with a structural dynamics model. A Taylor vortex is...
Saved in:
| Published in | Aerospace science and technology Vol. 74; pp. 112 - 119 |
|---|---|
| Main Authors | , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Masson SAS
01.03.2018
|
| Subjects | |
| Online Access | Get full text |
| ISSN | 1270-9638 1626-3219 |
| DOI | 10.1016/j.ast.2017.12.025 |
Cover
| Abstract | This article explores the evolution of the unsteady flow structure for rigid and elastically mounted NACA0012 airfoils subject to a parallel vortical gust disturbance at a Reynolds number of Re=150,000 using implicit large-eddy simulation coupled with a structural dynamics model. A Taylor vortex is supplied upstream of the airfoil and shown to be successful at eliciting laminar separation flutter in the elastically mounted system under conditions which normally require an artificial disturbance. Much of the gust-induced moment responsible for flutter excitation is supplied by a two-stage flow transition process on the undersurface of the wing after the gust passes the airfoil. The gust response triggers transition of the separated lower-surface boundary layer into spanwise coherent vortices followed by a laminar separation bubble accompanied by a secondary emergence of flow transition. These events appear to be analogous in some ways to the processes that appear during fully developed flutter but occur over a shorter timescale. |
|---|---|
| AbstractList | This article explores the evolution of the unsteady flow structure for rigid and elastically mounted NACA0012 airfoils subject to a parallel vortical gust disturbance at a Reynolds number of Re=150,000 using implicit large-eddy simulation coupled with a structural dynamics model. A Taylor vortex is supplied upstream of the airfoil and shown to be successful at eliciting laminar separation flutter in the elastically mounted system under conditions which normally require an artificial disturbance. Much of the gust-induced moment responsible for flutter excitation is supplied by a two-stage flow transition process on the undersurface of the wing after the gust passes the airfoil. The gust response triggers transition of the separated lower-surface boundary layer into spanwise coherent vortices followed by a laminar separation bubble accompanied by a secondary emergence of flow transition. These events appear to be analogous in some ways to the processes that appear during fully developed flutter but occur over a shorter timescale. |
| Author | Visbal, Miguel R. Barnes, Caleb J. |
| Author_xml | – sequence: 1 givenname: Caleb J. surname: Barnes fullname: Barnes, Caleb J. email: caleb.barnes.1@us.af.mil – sequence: 2 givenname: Miguel R. surname: Visbal fullname: Visbal, Miguel R. |
| BookMark | eNp9kEFLAzEUhINUsK3-AG_5A7sm2Sbb4EmKVqEgiB48hWz2RVLSpCSp0H9vip489PSGB98wMzM0CTEAQreUtJRQcbdtdS4tI7RvKWsJ4xdoSgUTTceonFTNetJI0S2v0CznLSGEyQWbos_1IRecIO9jyICjxcl9uRHrMGLw1dMZ7f0R7-IhFKh_l2x0PmNdsMYl6ZBdcTFoj9_gGKIfMw6H3QDpGl1a7TPc_N05-nh6fF89N5vX9cvqYdMYJvvScLCMdEwserGUGswgbScWkoNmhnMKwvBhMRBCeW_BEDFoLQcz9LzTdlzasZuj_tfXpJhzAquMK_qUqaZzXlGiTguprapt1GkhRZmqC1WS_iP3ye10Op5l7n8ZqJW-HSSVjYNgYHQJTFFjdGfoHztrgxc |
| CitedBy_id | crossref_primary_10_1016_j_jfluidstructs_2022_103828 crossref_primary_10_1016_j_jfluidstructs_2021_103425 crossref_primary_10_1016_j_jfluidstructs_2020_103138 crossref_primary_10_2514_1_J058654 crossref_primary_10_1016_j_jfluidstructs_2019_102767 crossref_primary_10_2514_1_J056711 crossref_primary_10_1063_5_0095681 crossref_primary_10_1016_j_ast_2019_06_044 crossref_primary_10_2514_1_J056914 crossref_primary_10_2514_1_J062272 crossref_primary_10_2514_1_J057262 |
| Cites_doi | 10.1016/0021-9991(81)90047-4 10.2514/2.591 10.1063/1.869867 10.2514/3.60901 10.1115/1.1517564 10.1016/0021-9991(92)90324-R 10.2514/3.23154 10.1080/10618562.2011.632374 10.1016/j.jfluidstructs.2007.11.005 10.1006/jfls.2000.0434 10.2514/2.2372 10.2514/3.9550 10.1146/annurev.fluid.30.1.199 10.1016/0021-9991(81)90156-X 10.1016/j.jfluidstructs.2011.05.009 10.2514/1.J052541 10.1002/fld.3725 10.2514/3.9340 10.1063/1.1586271 10.1016/j.jfluidstructs.2017.12.009 |
| ContentType | Journal Article |
| Copyright | 2018 |
| Copyright_xml | – notice: 2018 |
| DBID | AAYXX CITATION |
| DOI | 10.1016/j.ast.2017.12.025 |
| DatabaseName | CrossRef |
| DatabaseTitle | CrossRef |
| DatabaseTitleList | |
| DeliveryMethod | fulltext_linktorsrc |
| Discipline | Engineering |
| EISSN | 1626-3219 |
| EndPage | 119 |
| ExternalDocumentID | 10_1016_j_ast_2017_12_025 S1270963817315316 |
| 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- AATTM AAXKI AAYWO AAYXX ACLOT ACVFH ADCNI AEIPS AEUPX AFJKZ AFPUW AIGII AIIUN AKBMS AKRWK AKYEP ANKPU APXCP CITATION EFKBS ~HD |
| ID | FETCH-LOGICAL-c297t-5ef2032647689aecb9f36495ea2c551e6c5b4b00157fec06baa9bcb753afd8fd3 |
| IEDL.DBID | .~1 |
| ISSN | 1270-9638 |
| IngestDate | Wed Oct 29 21:25:04 EDT 2025 Thu Apr 24 23:04:17 EDT 2025 Fri Feb 23 02:33:23 EST 2024 |
| IsPeerReviewed | true |
| IsScholarly | true |
| Keywords | Aeroelastic Fluid–structure interaction Flutter Gust response Transitional Reynolds number |
| Language | English |
| LinkModel | DirectLink |
| MergedId | FETCHMERGED-LOGICAL-c297t-5ef2032647689aecb9f36495ea2c551e6c5b4b00157fec06baa9bcb753afd8fd3 |
| PageCount | 8 |
| ParticipantIDs | crossref_citationtrail_10_1016_j_ast_2017_12_025 crossref_primary_10_1016_j_ast_2017_12_025 elsevier_sciencedirect_doi_10_1016_j_ast_2017_12_025 |
| PublicationCentury | 2000 |
| PublicationDate | March 2018 2018-03-00 |
| PublicationDateYYYYMMDD | 2018-03-01 |
| PublicationDate_xml | – month: 03 year: 2018 text: March 2018 |
| PublicationDecade | 2010 |
| PublicationTitle | Aerospace science and technology |
| PublicationYear | 2018 |
| Publisher | Elsevier Masson SAS |
| Publisher_xml | – name: Elsevier Masson SAS |
| References | Gordnier, Visbal (br0090) June 2015 Poirel, Harris, Benaissa (br0010) 2008; 24 Alpert (br0190) 1981; 44 Barnes, Visbal (br0270) January 2016 Pulliam, Chaussee (br0130) 1981; 39 Gaitonde, Visbal (br0200) 1999 Mathew, Lechner, Foysi, Sesterhenn, Friedrich (br0250) 2003; 15 Rockwell (br0050) 1998; 30 Gaitonde, Visbal (br0110) 1998 Stolz, Adams (br0240) 1999; 11 Poirel, Mendes (br0020) 2014; 52 Lele (br0180) 1992; 103 Pulliam (br0170) 1986; 24 Taylor (br0290) 2010 Jameson, Schmidt, Turkel (br0160) 1981 Barnes, Visbal (br0310) June 2016 Rizzetta, Visbal (br0060) 2011; 25 Barnes, Visbal (br0300) June 2017 Visbal, Morgan, Rizzetta (br0220) June 2003 Morton, Melville, Visbal (br0260) 1998; 35 Visbal, Rizzetta (br0210) 2002; 124 Gordnier, Visbal (br0280) 2002; 16 Visbal, Gaitonde (br0100) 1999; 37 Rai, Chakravarthy (br0140) 1986; 24 Poirel, Métivier, Dumas (br0030) 2011; 27 Beam, Warming (br0120) 1978; 16 Barnes, Visbal (br0040) 2018; 77 Gordnier, Visbal (br0080) January 2015 Rai (br0150) 1989; 5 Garmann, Visbal, Orkwis (br0230) 2013; 71 Golubev, Nguyen, Visbal (br0070) January 2011 Poirel (10.1016/j.ast.2017.12.025_br0030) 2011; 27 Gordnier (10.1016/j.ast.2017.12.025_br0090) 2015 Gaitonde (10.1016/j.ast.2017.12.025_br0200) 1999 Gaitonde (10.1016/j.ast.2017.12.025_br0110) 1998 Golubev (10.1016/j.ast.2017.12.025_br0070) 2011 Gordnier (10.1016/j.ast.2017.12.025_br0080) 2015 Rai (10.1016/j.ast.2017.12.025_br0150) 1989; 5 Mathew (10.1016/j.ast.2017.12.025_br0250) 2003; 15 Rockwell (10.1016/j.ast.2017.12.025_br0050) 1998; 30 Morton (10.1016/j.ast.2017.12.025_br0260) 1998; 35 Poirel (10.1016/j.ast.2017.12.025_br0020) 2014; 52 Pulliam (10.1016/j.ast.2017.12.025_br0170) 1986; 24 Barnes (10.1016/j.ast.2017.12.025_br0300) 2017 Barnes (10.1016/j.ast.2017.12.025_br0310) 2016 Lele (10.1016/j.ast.2017.12.025_br0180) 1992; 103 Gordnier (10.1016/j.ast.2017.12.025_br0280) 2002; 16 Stolz (10.1016/j.ast.2017.12.025_br0240) 1999; 11 Barnes (10.1016/j.ast.2017.12.025_br0270) 2016 Beam (10.1016/j.ast.2017.12.025_br0120) 1978; 16 Pulliam (10.1016/j.ast.2017.12.025_br0130) 1981; 39 Poirel (10.1016/j.ast.2017.12.025_br0010) 2008; 24 Visbal (10.1016/j.ast.2017.12.025_br0100) 1999; 37 Garmann (10.1016/j.ast.2017.12.025_br0230) 2013; 71 Visbal (10.1016/j.ast.2017.12.025_br0220) 2003 Visbal (10.1016/j.ast.2017.12.025_br0210) 2002; 124 Barnes (10.1016/j.ast.2017.12.025_br0040) 2018; 77 Rizzetta (10.1016/j.ast.2017.12.025_br0060) 2011; 25 Jameson (10.1016/j.ast.2017.12.025_br0160) 1981 Rai (10.1016/j.ast.2017.12.025_br0140) 1986; 24 Taylor (10.1016/j.ast.2017.12.025_br0290) 2010 Alpert (10.1016/j.ast.2017.12.025_br0190) 1981; 44 |
| References_xml | – volume: 24 start-page: 735 year: 1986 end-page: 743 ident: br0140 article-title: An implicit form for the Osher upwind scheme publication-title: AIAA J. – volume: 44 start-page: 212 year: 1981 end-page: 219 ident: br0190 article-title: Implicit filtering in conjunction with explicit filtering publication-title: J. Comput. Phys. – volume: 27 start-page: 1262 year: 2011 end-page: 1277 ident: br0030 article-title: Computational aeroelastic simulations of self-sustained pitch oscillations of a NACA0012 at transitional Reynolds numbers publication-title: J. Fluids Struct. – volume: 25 start-page: 509 year: 2011 end-page: 533 ident: br0060 article-title: Exploration of plasma-based control for low-Reynolds number airfoil gust interaction publication-title: Int. J. Comput. Fluid Dyn. – year: 1998 ident: br0110 article-title: High-Order Schemes for Navier–Stokes Equations: Algorithm and Implementation into FDL3DI – volume: 35 start-page: 798 year: 1998 end-page: 805 ident: br0260 article-title: Accuracy and coupling issues of aeroelastic Navier–Stokes solutions on deforming meshes publication-title: J. Aircr. – volume: 24 start-page: 1931 year: 1986 end-page: 1940 ident: br0170 article-title: Artificial dissipation models for the Euler equations publication-title: AIAA J. – volume: 124 start-page: 836 year: 2002 end-page: 847 ident: br0210 article-title: Large-eddy simulation on curvilinear grids using compact differencing and filtering schemes publication-title: J. Fluids Eng. – volume: 71 start-page: 1546 year: 2013 end-page: 1565 ident: br0230 article-title: Comparative study of implicit and subgrid-scale model large-eddy simulation techniques for low-Reynolds number airfoil applications publication-title: Int. J. Numer. Methods Fluids – volume: 11 start-page: 1699 year: 1999 end-page: 1701 ident: br0240 article-title: An approximate deconvolution procedure for large-eddy simulation publication-title: Phys. Fluids – year: 1999 ident: br0200 article-title: Further Development of a Navier–Stokes Solution Procedure Based on Higher-Order Formulas – volume: 16 start-page: 393 year: 1978 end-page: 402 ident: br0120 article-title: An implicit factored scheme for the compressible Navier–Stokes equations publication-title: AIAA J. – volume: 15 start-page: 2279 year: 2003 end-page: 2289 ident: br0250 article-title: An explicit filtering method for large eddy simulation of compressible flows publication-title: Phys. Fluids – start-page: 96 year: 2010 end-page: 101 ident: br0290 article-title: On the dissipation of eddies publication-title: The Scientific Papers of Sir Geoffrey Ingram Taylor, Vol. 2: Meteorology, Oceanography, and Turbulent Flow – volume: 5 start-page: 305 year: 1989 end-page: 311 ident: br0150 article-title: Three-dimensional Navier–Stokes simulations of turbine rotor–stator interaction, part i – methodology publication-title: J. Propuls. Power – volume: 77 start-page: 213 year: 2018 end-page: 230 ident: br0040 article-title: On the role of flow transition in laminar separation flutter publication-title: J. Fluids Struct. – year: 1981 ident: br0160 article-title: Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge–Kutta Time Stepping Schemes – volume: 103 start-page: 16 year: 1992 end-page: 42 ident: br0180 article-title: Compact finite difference schemes with spectral-like resolution publication-title: J. Comput. Phys. – volume: 39 start-page: 347 year: 1981 end-page: 363 ident: br0130 article-title: A diagonal form of an implicit approximate-factorization algorithm publication-title: J. Comput. Phys. – year: January 2016 ident: br0270 article-title: High Fidelity LES Simulations of Self-Sustained Pitching Oscillations on a NACA0012 Airfoil at Transitional Reynolds Numbers – volume: 30 start-page: 199 year: 1998 end-page: 229 ident: br0050 article-title: Vortex–body interactions publication-title: Annu. Rev. Fluid Mech. – year: June 2017 ident: br0300 article-title: Effects of Vertical Position and Orientation on a Vortical-Gust/Airfoil Interaction at a Transitional Reynolds Number – volume: 16 start-page: 497 year: 2002 end-page: 527 ident: br0280 article-title: Development of a three-dimensional viscous aeroelastic solver for nonlinear panel flutter publication-title: J. Fluids Struct. – volume: 37 start-page: 1231 year: 1999 end-page: 1239 ident: br0100 article-title: High-order-accurate methods for complex unsteady subsonic flows publication-title: AIAA J. – year: June 2016 ident: br0310 article-title: Aeroelastic Response of an Airfoil at Transitional Reynolds Numbers – year: June 2015 ident: br0090 article-title: Impact of Vortical Gust on the Aerodynamics of a Finite Aspect-Ratio Wing – year: January 2015 ident: br0080 article-title: Implicit LES Computation of a Vortical-Gust/Wing Interaction for Transitional Flow – year: June 2003 ident: br0220 article-title: An Implicit LES Approach Based on High-Order Compact Differencing and Filtering Schemes – volume: 52 start-page: 1581 year: 2014 end-page: 1590 ident: br0020 article-title: Experimental small-amplitude self-sustained pitch-heave oscillations at transitional Reynolds numbers publication-title: AIAA J. – volume: 24 start-page: 700 year: 2008 end-page: 719 ident: br0010 article-title: Self-sustained aeroelastic oscillations of a NACA 0012 airfoil at low-to-moderate Reynolds numbers publication-title: J. Fluids Struct. – year: January 2011 ident: br0070 article-title: High Fidelity Simulations of a Transitional Airfoil Interacting with Upstream Vortical Structure – volume: 44 start-page: 212 issue: 1 year: 1981 ident: 10.1016/j.ast.2017.12.025_br0190 article-title: Implicit filtering in conjunction with explicit filtering publication-title: J. Comput. Phys. doi: 10.1016/0021-9991(81)90047-4 – volume: 37 start-page: 1231 issue: 10 year: 1999 ident: 10.1016/j.ast.2017.12.025_br0100 article-title: High-order-accurate methods for complex unsteady subsonic flows publication-title: AIAA J. doi: 10.2514/2.591 – volume: 11 start-page: 1699 issue: 7 year: 1999 ident: 10.1016/j.ast.2017.12.025_br0240 article-title: An approximate deconvolution procedure for large-eddy simulation publication-title: Phys. Fluids doi: 10.1063/1.869867 – volume: 16 start-page: 393 issue: 4 year: 1978 ident: 10.1016/j.ast.2017.12.025_br0120 article-title: An implicit factored scheme for the compressible Navier–Stokes equations publication-title: AIAA J. doi: 10.2514/3.60901 – volume: 124 start-page: 836 issue: 4 year: 2002 ident: 10.1016/j.ast.2017.12.025_br0210 article-title: Large-eddy simulation on curvilinear grids using compact differencing and filtering schemes publication-title: J. Fluids Eng. doi: 10.1115/1.1517564 – year: 2016 ident: 10.1016/j.ast.2017.12.025_br0270 – volume: 103 start-page: 16 issue: 1 year: 1992 ident: 10.1016/j.ast.2017.12.025_br0180 article-title: Compact finite difference schemes with spectral-like resolution publication-title: J. Comput. Phys. doi: 10.1016/0021-9991(92)90324-R – volume: 5 start-page: 305 issue: 3 year: 1989 ident: 10.1016/j.ast.2017.12.025_br0150 article-title: Three-dimensional Navier–Stokes simulations of turbine rotor–stator interaction, part i – methodology publication-title: J. Propuls. Power doi: 10.2514/3.23154 – volume: 25 start-page: 509 issue: 10 year: 2011 ident: 10.1016/j.ast.2017.12.025_br0060 article-title: Exploration of plasma-based control for low-Reynolds number airfoil gust interaction publication-title: Int. J. Comput. Fluid Dyn. doi: 10.1080/10618562.2011.632374 – volume: 24 start-page: 700 issue: 5 year: 2008 ident: 10.1016/j.ast.2017.12.025_br0010 article-title: Self-sustained aeroelastic oscillations of a NACA 0012 airfoil at low-to-moderate Reynolds numbers publication-title: J. Fluids Struct. doi: 10.1016/j.jfluidstructs.2007.11.005 – year: 1981 ident: 10.1016/j.ast.2017.12.025_br0160 – volume: 16 start-page: 497 issue: 4 year: 2002 ident: 10.1016/j.ast.2017.12.025_br0280 article-title: Development of a three-dimensional viscous aeroelastic solver for nonlinear panel flutter publication-title: J. Fluids Struct. doi: 10.1006/jfls.2000.0434 – volume: 35 start-page: 798 issue: 5 year: 1998 ident: 10.1016/j.ast.2017.12.025_br0260 article-title: Accuracy and coupling issues of aeroelastic Navier–Stokes solutions on deforming meshes publication-title: J. Aircr. doi: 10.2514/2.2372 – year: 2011 ident: 10.1016/j.ast.2017.12.025_br0070 – volume: 24 start-page: 1931 issue: 12 year: 1986 ident: 10.1016/j.ast.2017.12.025_br0170 article-title: Artificial dissipation models for the Euler equations publication-title: AIAA J. doi: 10.2514/3.9550 – start-page: 96 year: 2010 ident: 10.1016/j.ast.2017.12.025_br0290 article-title: On the dissipation of eddies – year: 2003 ident: 10.1016/j.ast.2017.12.025_br0220 – year: 2017 ident: 10.1016/j.ast.2017.12.025_br0300 – volume: 30 start-page: 199 year: 1998 ident: 10.1016/j.ast.2017.12.025_br0050 article-title: Vortex–body interactions publication-title: Annu. Rev. Fluid Mech. doi: 10.1146/annurev.fluid.30.1.199 – year: 2015 ident: 10.1016/j.ast.2017.12.025_br0080 – year: 2016 ident: 10.1016/j.ast.2017.12.025_br0310 – volume: 39 start-page: 347 issue: 2 year: 1981 ident: 10.1016/j.ast.2017.12.025_br0130 article-title: A diagonal form of an implicit approximate-factorization algorithm publication-title: J. Comput. Phys. doi: 10.1016/0021-9991(81)90156-X – volume: 27 start-page: 1262 year: 2011 ident: 10.1016/j.ast.2017.12.025_br0030 article-title: Computational aeroelastic simulations of self-sustained pitch oscillations of a NACA0012 at transitional Reynolds numbers publication-title: J. Fluids Struct. doi: 10.1016/j.jfluidstructs.2011.05.009 – volume: 52 start-page: 1581 issue: 8 year: 2014 ident: 10.1016/j.ast.2017.12.025_br0020 article-title: Experimental small-amplitude self-sustained pitch-heave oscillations at transitional Reynolds numbers publication-title: AIAA J. doi: 10.2514/1.J052541 – volume: 71 start-page: 1546 issue: 12 year: 2013 ident: 10.1016/j.ast.2017.12.025_br0230 article-title: Comparative study of implicit and subgrid-scale model large-eddy simulation techniques for low-Reynolds number airfoil applications publication-title: Int. J. Numer. Methods Fluids doi: 10.1002/fld.3725 – year: 1999 ident: 10.1016/j.ast.2017.12.025_br0200 – year: 2015 ident: 10.1016/j.ast.2017.12.025_br0090 – volume: 24 start-page: 735 issue: 5 year: 1986 ident: 10.1016/j.ast.2017.12.025_br0140 article-title: An implicit form for the Osher upwind scheme publication-title: AIAA J. doi: 10.2514/3.9340 – year: 1998 ident: 10.1016/j.ast.2017.12.025_br0110 – volume: 15 start-page: 2279 issue: 8 year: 2003 ident: 10.1016/j.ast.2017.12.025_br0250 article-title: An explicit filtering method for large eddy simulation of compressible flows publication-title: Phys. Fluids doi: 10.1063/1.1586271 – volume: 77 start-page: 213 year: 2018 ident: 10.1016/j.ast.2017.12.025_br0040 article-title: On the role of flow transition in laminar separation flutter publication-title: J. Fluids Struct. doi: 10.1016/j.jfluidstructs.2017.12.009 |
| SSID | ssj0002942 |
| Score | 2.2547839 |
| Snippet | This article explores the evolution of the unsteady flow structure for rigid and elastically mounted NACA0012 airfoils subject to a parallel vortical gust... |
| SourceID | crossref elsevier |
| SourceType | Enrichment Source Index Database Publisher |
| StartPage | 112 |
| SubjectTerms | Aeroelastic Fluid–structure interaction Flutter Gust response Transitional Reynolds number |
| Title | Gust response of rigid and elastically mounted airfoils at a transitional Reynolds number |
| URI | https://dx.doi.org/10.1016/j.ast.2017.12.025 |
| Volume | 74 |
| hasFullText | 1 |
| inHoldings | 1 |
| isFullTextHit | |
| isPrint | |
| journalDatabaseRights | – providerCode: PRVESC databaseName: Baden-Württemberg Complete Freedom Collection (Elsevier) customDbUrl: eissn: 1626-3219 dateEnd: 99991231 omitProxy: true ssIdentifier: ssj0002942 issn: 1270-9638 databaseCode: GBLVA dateStart: 20110101 isFulltext: true titleUrlDefault: https://www.sciencedirect.com providerName: Elsevier – providerCode: PRVESC databaseName: Elsevier ScienceDirect Freedom Collection Journals customDbUrl: eissn: 1626-3219 dateEnd: 99991231 omitProxy: true ssIdentifier: ssj0002942 issn: 1270-9638 databaseCode: AIKHN dateStart: 19970101 isFulltext: true titleUrlDefault: https://www.sciencedirect.com providerName: Elsevier – providerCode: PRVESC databaseName: Elsevier SD Complete Freedom Collection [SCCMFC] customDbUrl: eissn: 1626-3219 dateEnd: 99991231 omitProxy: true ssIdentifier: ssj0002942 issn: 1270-9638 databaseCode: ACRLP dateStart: 19970101 isFulltext: true titleUrlDefault: https://www.sciencedirect.com providerName: Elsevier – providerCode: PRVESC databaseName: Elsevier SD Freedom Collection customDbUrl: eissn: 1626-3219 dateEnd: 99991231 omitProxy: true ssIdentifier: ssj0002942 issn: 1270-9638 databaseCode: .~1 dateStart: 19970101 isFulltext: true titleUrlDefault: https://www.sciencedirect.com providerName: Elsevier – providerCode: PRVLSH databaseName: Elsevier Journals customDbUrl: mediaType: online eissn: 1626-3219 dateEnd: 99991231 omitProxy: true ssIdentifier: ssj0002942 issn: 1270-9638 databaseCode: AKRWK dateStart: 19970101 isFulltext: true providerName: Library Specific Holdings |
| link | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwnV1LS8NAEF5KvehBfGJ9sQdPQmyTbF7HUqxVsQe1UE9hnxCJSWnTQy_-dmfy0ArqQQiBLLMhmUxmv9mdnY-QC44o1zfSUsxXFhNwCo3HwJaFGzpKBNzgfueHsT-asLupN22RQbMXBtMqa99f-fTSW9ct3Vqb3VmSdJ9wzRTNxw5c-G1tLLvNWIAsBlfvX2keTlQS6KCwhdLNymaZ48UXmE5pB-WMILJl_zQ2rY03wx2yXQNF2q-eZZe0dLZHttbKB-6Tl5vloqDzKstV09xQZLlSlGeKakDF5TR1uqJvyAehoT2ZmzxJF5QXlNMCR6mkmgqkj3qV5ala0Ioh5IBMhtfPg5FVUyVY0omCwvK0QSp0n0H0EHEtRWRcH2IfzR0JmEj70hOsBEiB0bLnC84jIQXEKvAtQqPcQ9LO8kwfEYoQSkUhZ6EjIRyCw3WZgzcEdMB7YYf0GiXFsq4jjnQWadwkjL3G8IYx6jW2nRj02iGXn11mVRGNv4RZo_n4myXE4OR_73b8v24nZBOuwiqr7JS0i_lSnwHMKMR5aUfnZKN_ez8afwANZtJF |
| linkProvider | Elsevier |
| linkToHtml | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwnV07T8MwELZKGYAB8RTl6YEJKbRNnNeIKkqBtgO0Upks27GloJJWbTp04bdzlwcUCRiQogyOHSWXy_k7-7M_Qi4FolzPKCtiXmQxCafAuAx8WTqBHUlfGFzv3Ot7nSF7GLmjCmmVa2GQVlnE_jymZ9G6KKkX1qxP47j-jHOm6D5N34HftumtkXXm2j5mYNfvXzwPO8wUdLC2hdXLqc2M5CXmyKds-tmQIMpl_9Q5rXQ47R2yXSBFepM_zC6p6GSPbK3sH7hPXu4W85TOcpqrphNDUeYqoiKJqAZYnI1Tj5f0DQUhNJTHMzOJx3MqUipoit1UnI8F0ie9TCbjaE5ziZADMmzfDlodq9BKsJQd-qnlaoNa6B6D9CEUWsnQOB4kP1rYCkCR9pQrWYaQfKNVw5NChFJJSFbgYwQmcg5JNZkk-ohQxFBRGAgW2AryITgch9l4Q4AHohHUSKM0ElfFRuKoZzHmJWPslcMbcrQrb9oc7FojV59NpvkuGn9VZqXl-TdX4BDlf292_L9mF2SjM-h1efe-_3hCNuFKkFPMTkk1nS30GWCOVJ5nPvUBFsnT2g |
| 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=Gust+response+of+rigid+and+elastically+mounted+airfoils+at+a+transitional+Reynolds+number&rft.jtitle=Aerospace+science+and+technology&rft.au=Barnes%2C+Caleb+J.&rft.au=Visbal%2C+Miguel+R.&rft.date=2018-03-01&rft.issn=1270-9638&rft.volume=74&rft.spage=112&rft.epage=119&rft_id=info:doi/10.1016%2Fj.ast.2017.12.025&rft.externalDBID=n%2Fa&rft.externalDocID=10_1016_j_ast_2017_12_025 |
| 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 |