{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,12,31]],"date-time":"2025-12-31T12:17:19Z","timestamp":1767183439449},"reference-count":22,"publisher":"Springer Science and Business Media LLC","issue":"7","license":[{"start":{"date-parts":[[2013,6,23]],"date-time":"2013-06-23T00:00:00Z","timestamp":1371945600000},"content-version":"tdm","delay-in-days":0,"URL":"http:\/\/www.springer.com\/tdm"}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["Exp Fluids"],"published-print":{"date-parts":[[2013,7]]},"DOI":"10.1007\/s00348-013-1564-9","type":"journal-article","created":{"date-parts":[[2013,6,22]],"date-time":"2013-06-22T15:08:31Z","timestamp":1371913711000},"source":"Crossref","is-referenced-by-count":5,"title":["Passive control of unsteady-wing tip vortex via a slender half-delta wing in both reverse and regular configurations"],"prefix":"10.1007","volume":"54","author":[{"given":"T.","family":"Lee","sequence":"first","affiliation":[]},{"given":"J.","family":"Pereira","sequence":"additional","affiliation":[]}],"member":"297","published-online":{"date-parts":[[2013,6,23]]},"reference":[{"issue":"5","key":"1564_CR1","doi-asserted-by":"publisher","first-page":"1138","DOI":"10.2514\/1.2707","volume":"41","author":"D Birch","year":"2004","unstructured":"Birch D, Lee T (2004) The structure and induced drag of a tip vortex. J Aircraft 41(5):1138\u20131145","journal-title":"J Aircraft"},{"issue":"1","key":"1564_CR2","doi-asserted-by":"publisher","first-page":"175","DOI":"10.2514\/1.37307","volume":"46","author":"C Breitsamter","year":"2009","unstructured":"Breitsamter C, Allen A (2009) Transport aircraft wake influenced by oscillating winglet flaps. J Aircraft 46(1):175\u2013188","journal-title":"J Aircraft"},{"key":"1564_CR3","doi-asserted-by":"publisher","first-page":"1092","DOI":"10.2514\/2.1072","volume":"38","author":"JW Chang","year":"2000","unstructured":"Chang JW, Park SO (2000) Measurement in the tip vortex roll-up region of an oscillating wing. AIAA J 38:1092\u20131095","journal-title":"AIAA J"},{"key":"1564_CR4","doi-asserted-by":"publisher","first-page":"151","DOI":"10.1016\/S0889-9746(87)90315-X","volume":"1","author":"SH Chen","year":"1987","unstructured":"Chen SH, Ho CM (1987) Near wake of an unsteady symmetric airfoil. J Fluids Struct 1:151\u2013164","journal-title":"J Fluids Struct"},{"key":"1564_CR5","doi-asserted-by":"crossref","unstructured":"Duraisamy K, Baeder JD (2003) Control of tip vortex structure using steady and oscillatory blowing. AIAA Paper 2003\u20133407","DOI":"10.2514\/6.2003-3407"},{"key":"1564_CR6","doi-asserted-by":"publisher","first-page":"1","DOI":"10.1016\/S0889-9746(88)90116-8","volume":"2","author":"LE Ericsson","year":"1988","unstructured":"Ericsson LE, Redding JP (1988) Fluid mechanics of dynamic stall. Part I. Unsteady flow concept. J Fluids Struct 2:1\u201333","journal-title":"J Fluids Struct"},{"key":"1564_CR7","doi-asserted-by":"publisher","first-page":"305","DOI":"10.1007\/BF00189488","volume":"14","author":"TJ Gieseke","year":"1993","unstructured":"Gieseke TJ, Guezennec YG (1993) An experimental approach to the calibration and use of triple hot-wire probes. Exp Fluids 14:305\u2013315","journal-title":"Exp Fluids"},{"issue":"2","key":"1564_CR8","doi-asserted-by":"publisher","first-page":"375","DOI":"10.2514\/1.J051123","volume":"50","author":"D Greenblatt","year":"2012","unstructured":"Greenblatt D (2012) Fluidic control of a wing tip vortex. AIAA J 50(2):375\u2013386","journal-title":"AIAA J"},{"issue":"2","key":"1564_CR9","doi-asserted-by":"publisher","first-page":"2845","DOI":"10.2514\/1.41767","volume":"47","author":"D Greenblatt","year":"2009","unstructured":"Greenblatt D, Vey S, Paschereit OC, Meyer R (2009) Flap vortex management using active Gurney flaps. AIAA J 47(2):2845\u20132856","journal-title":"AIAA J"},{"issue":"2","key":"1564_CR10","doi-asserted-by":"publisher","first-page":"120","DOI":"10.2514\/3.45428","volume":"24","author":"JC Hardin","year":"1987","unstructured":"Hardin JC, Lamkin SL (1987) Concepts for reduction of blade\/vortex interaction noise. J Aircraft 24(2):120\u2013125","journal-title":"J Aircraft"},{"issue":"6","key":"1564_CR11","doi-asserted-by":"crossref","first-page":"419","DOI":"10.1299\/jfst.6.976","volume":"6","author":"H Hasebe","year":"2011","unstructured":"Hasebe H, Naka Y, Fukagata K (2011) An attempt for suppression of wing-tip vortex using plasma actuators. J Fluid Sci Tech 6(6):419\u2013437","journal-title":"J Fluid Sci Tech"},{"key":"1564_CR12","doi-asserted-by":"publisher","first-page":"108","DOI":"10.1007\/s003480050214","volume":"25","author":"T Lee","year":"1998","unstructured":"Lee T, Basu S (1998) Investigation of unsteady boundary layer developing on an oscillating airfoil. Exp Fluids 25:108\u2013117","journal-title":"Exp Fluids"},{"issue":"6","key":"1564_CR13","doi-asserted-by":"publisher","first-page":"1946","DOI":"10.2514\/1.C000225","volume":"47","author":"T Lee","year":"2010","unstructured":"Lee T, Pereira J (2010) On the nature of wake- and jet-like axial tip-vortex flow. J Aircraft 47(6):1946\u20131954","journal-title":"J Aircraft"},{"issue":"6","key":"1564_CR14","doi-asserted-by":"publisher","first-page":"1593","DOI":"10.1007\/s00348-012-1274-8","volume":"52","author":"T Lee","year":"2012","unstructured":"Lee T, Su YY (2012) Wingtip vortex control via the use of a reverse half-delta wing. Exp Fluids 52(6):1593\u20131609","journal-title":"Exp Fluids"},{"issue":"4","key":"1564_CR15","doi-asserted-by":"publisher","first-page":"832","DOI":"10.2514\/3.46798","volume":"32","author":"MV Lowson","year":"1995","unstructured":"Lowson MV, Riley AJ (1995) Vortex breakdown control by delta wing geometry. J Aircraft 32(4):832\u2013838","journal-title":"J Aircraft"},{"issue":"2","key":"1564_CR16","doi-asserted-by":"publisher","first-page":"321","DOI":"10.2514\/1.25956","volume":"45","author":"CG Matalanis","year":"2007","unstructured":"Matalanis CG, Eaton JK (2007a) Wake vortex control using static segmented Gurney flaps. AIAA J 45(2):321\u2013328","journal-title":"AIAA J"},{"issue":"8","key":"1564_CR17","doi-asserted-by":"publisher","first-page":"1847","DOI":"10.2514\/1.28319","volume":"45","author":"CG Matalanis","year":"2007","unstructured":"Matalanis CG, Eaton JK (2007b) Wake vortex control using rapidly actuated segmented Gurney flaps. AIAA J 45(8):1847\u20131884","journal-title":"AIAA J"},{"key":"1564_CR18","doi-asserted-by":"publisher","first-page":"3","DOI":"10.1016\/0894-1777(88)90043-X","volume":"1","author":"RJ Moffat","year":"1985","unstructured":"Moffat RJ (1985) Describing the uncertainties in experimental results. Exp Thermal Fluid Sci 1:3\u201317","journal-title":"Exp Thermal Fluid Sci"},{"issue":"5","key":"1564_CR19","doi-asserted-by":"publisher","first-page":"880","DOI":"10.2514\/3.47030","volume":"33","author":"R Rennie","year":"1996","unstructured":"Rennie R, Jumper EJ (1996) Experimental measurements of dynamic control surface effectiveness. J Aircraft 33(5):880\u2013887","journal-title":"J Aircraft"},{"key":"1564_CR20","doi-asserted-by":"publisher","first-page":"507","DOI":"10.1016\/S0376-0421(99)00006-8","volume":"35","author":"V Rossow","year":"1999","unstructured":"Rossow V (1999) Lift-generated vortex wake of subsonic transport aircraft. Prog Aero Sci 35:507\u2013660","journal-title":"Prog Aero Sci"},{"key":"1564_CR21","doi-asserted-by":"publisher","first-page":"107","DOI":"10.1146\/annurev.fluid.30.1.107","volume":"30","author":"PR Spalart","year":"1998","unstructured":"Spalart PR (1998) Airplane trailing vortices. Ann Rev Fluid Mech 30:107\u2013138","journal-title":"Ann Rev Fluid Mech"},{"issue":"3","key":"1564_CR22","doi-asserted-by":"publisher","first-page":"749","DOI":"10.2514\/1.40615","volume":"47","author":"K Taira","year":"2009","unstructured":"Taira K, Colonius T (2009) Effect of tip vortices in low-Reynolds-number poststall flow control. AIAA J 47(3):749\u2013755","journal-title":"AIAA J"}],"container-title":["Experiments in Fluids"],"original-title":[],"language":"en","link":[{"URL":"http:\/\/link.springer.com\/content\/pdf\/10.1007\/s00348-013-1564-9.pdf","content-type":"application\/pdf","content-version":"vor","intended-application":"text-mining"},{"URL":"http:\/\/link.springer.com\/article\/10.1007\/s00348-013-1564-9\/fulltext.html","content-type":"text\/html","content-version":"vor","intended-application":"text-mining"},{"URL":"http:\/\/link.springer.com\/content\/pdf\/10.1007\/s00348-013-1564-9","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"},{"URL":"http:\/\/link.springer.com\/content\/pdf\/10.1007\/s00348-013-1564-9.pdf","content-type":"application\/pdf","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2019,5,28]],"date-time":"2019-05-28T14:10:29Z","timestamp":1559052629000},"score":1,"resource":{"primary":{"URL":"http:\/\/link.springer.com\/10.1007\/s00348-013-1564-9"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2013,6,23]]},"references-count":22,"journal-issue":{"issue":"7","published-print":{"date-parts":[[2013,7]]}},"alternative-id":["1564"],"URL":"https:\/\/doi.org\/10.1007\/s00348-013-1564-9","relation":{},"ISSN":["0723-4864","1432-1114"],"issn-type":[{"value":"0723-4864","type":"print"},{"value":"1432-1114","type":"electronic"}],"subject":[],"published":{"date-parts":[[2013,6,23]]},"article-number":"1564"}}