{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,9,10]],"date-time":"2025-09-10T22:34:02Z","timestamp":1757543642337,"version":"3.37.3"},"reference-count":28,"publisher":"Springer Science and Business Media LLC","issue":"5","license":[{"start":{"date-parts":[[2022,5,10]],"date-time":"2022-05-10T00:00:00Z","timestamp":1652140800000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/www.springer.com\/tdm"},{"start":{"date-parts":[[2022,5,10]],"date-time":"2022-05-10T00:00:00Z","timestamp":1652140800000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/www.springer.com\/tdm"}],"funder":[{"DOI":"10.13039\/501100001809","name":"National Natural Science Foundation of China","doi-asserted-by":"publisher","award":["11972017"],"award-info":[{"award-number":["11972017"]}],"id":[{"id":"10.13039\/501100001809","id-type":"DOI","asserted-by":"publisher"}]}],"content-domain":{"domain":["link.springer.com"],"crossmark-restriction":false},"short-container-title":["J Vis"],"published-print":{"date-parts":[[2022,10]]},"DOI":"10.1007\/s12650-022-00841-y","type":"journal-article","created":{"date-parts":[[2022,5,10]],"date-time":"2022-05-10T17:03:04Z","timestamp":1652202184000},"page":"967-981","update-policy":"https:\/\/doi.org\/10.1007\/springer_crossmark_policy","source":"Crossref","is-referenced-by-count":6,"title":["Experimental investigation on the transient process of jet deflection controlled by passive secondary flow"],"prefix":"10.1007","volume":"25","author":[{"given":"Nanxing","family":"Shi","sequence":"first","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"ORCID":"https:\/\/orcid.org\/0000-0002-3469-0092","authenticated-orcid":false,"given":"Yunsong","family":"Gu","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Yuhang","family":"Zhou","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Yi","family":"Wang","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Zhao","family":"Li","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]}],"member":"297","published-online":{"date-parts":[[2022,5,10]]},"reference":[{"issue":"10","key":"841_CR1","doi-asserted-by":"publisher","first-page":"1719","DOI":"10.1063\/1.863642","volume":"25","author":"HH Bau","year":"1982","unstructured":"Bau HH (1982) Kelvin-Helmholtz instability for parallel flow in porous media: a linear theory. Phys Fluids 25(10):1719\u20131722. https:\/\/doi.org\/10.1063\/1.863642","journal-title":"Phys Fluids"},{"issue":"3","key":"841_CR2","doi-asserted-by":"publisher","first-page":"201","DOI":"10.1017\/s0001925900001797","volume":"11","author":"C Bourque","year":"1960","unstructured":"Bourque C, Newman BG (1960) Reattachment of a two-dimensional, incompressible jet to an adjacent flat plate. Aeronaut Quarterly 11(3):201\u2013232. https:\/\/doi.org\/10.1017\/s0001925900001797","journal-title":"Aeronaut Quarterly"},{"key":"841_CR3","doi-asserted-by":"publisher","first-page":"397","DOI":"10.1017\/S0022112082003401","volume":"125","author":"JE Broadwell","year":"1982","unstructured":"Broadwell JE, Breidenthal RE (1982) A simple model of mixing and chemical reaction in a turbulent shear layer. J Fluid Mech 125:397\u2013410. https:\/\/doi.org\/10.1017\/S0022112082003401","journal-title":"J Fluid Mech"},{"key":"841_CR4","doi-asserted-by":"publisher","DOI":"10.2514\/6.1998-3255","author":"JD Flamm","year":"1998","unstructured":"Flamm JD (1998) Experimental study of a nozzle using fluidic counterflow for thrust vectoring. AIAA. https:\/\/doi.org\/10.2514\/6.1998-3255","journal-title":"AIAA"},{"issue":"10","key":"841_CR5","doi-asserted-by":"publisher","DOI":"10.7527\/S1000-6893.2019.23609","volume":"41","author":"DS Gong","year":"2020","unstructured":"Gong DS, Gu YS, Zhou YH, Shi NX (2020) Control law of passive fluid thrust vector nozzle based on thermal jet of micro turbojet engine. Acta Aeronaut Astronaut Sin 41(10):123609. https:\/\/doi.org\/10.7527\/S1000-6893.2019.23609","journal-title":"Acta Aeronaut Astronaut Sin"},{"key":"841_CR6","doi-asserted-by":"crossref","unstructured":"Levin SG, Manion FM (1962) Jet Attachment Distance as a Function of Adjacent Wall Offset and Angle. HDL-TR-1087","DOI":"10.21236\/AD0297895"},{"issue":"2","key":"841_CR7","doi-asserted-by":"publisher","first-page":"19","DOI":"10.3969\/j.issn.1673-4599.2008.02.005","volume":"28","author":"YJ Lian","year":"2008","unstructured":"Lian YJ (2008) Fluidic thrust vectoring techniques research. Aircr Des 28(2):19\u201324. https:\/\/doi.org\/10.3969\/j.issn.1673-4599.2008.02.005","journal-title":"Aircr Des"},{"issue":"12","key":"841_CR8","doi-asserted-by":"publisher","first-page":"1964","DOI":"10.2514\/3.9554","volume":"24","author":"TS Lund","year":"1986","unstructured":"Lund TS (1986) Augmented thrust and mass flow associated with two-dimensional jet reattachment. AIAA J 24(12):1964\u20131970. https:\/\/doi.org\/10.2514\/3.9554","journal-title":"AIAA J"},{"issue":"2514\/1","key":"841_CR9","first-page":"J059696","volume":"10","author":"Y Maruyama","year":"2021","unstructured":"Maruyama Y, Sakata M, Takahashi Y (2021) Performance analyses of fluidic thrust vector control system using dual throat nozzle. AIAA J 10(2514\/1):J059696","journal-title":"AIAA J"},{"key":"841_CR10","unstructured":"Nasr A, Lai JCS (2000) The effects of wall inclination on an inclined offset jet. In: 10th International symposium applications of laser techniques to fluid mechanics"},{"key":"841_CR11","doi-asserted-by":"publisher","unstructured":"Nasr A, Lai JCS, Siah O, Young J (2006) Flow characteristics of an inclined offset jet. In: 36th AIAA fluid dynamics conference and exhibit. https:\/\/doi.org\/10.2514\/6.2006-3372","DOI":"10.2514\/6.2006-3372"},{"issue":"1","key":"841_CR12","doi-asserted-by":"publisher","first-page":"47","DOI":"10.1007\/s003480050149","volume":"24","author":"A Nasr","year":"1998","unstructured":"Nasr A, Lai JCS (1998) A turbulent plane offset jet with small offset ratio. Exp Fluids 24(1):47\u201357. https:\/\/doi.org\/10.1007\/s003480050149","journal-title":"Exp Fluids"},{"issue":"165","key":"841_CR13","doi-asserted-by":"publisher","first-page":"340","DOI":"10.1299\/jsme1958.22.340","volume":"22","author":"T Nozaki","year":"1979","unstructured":"Nozaki T, Hatta K, Nakashima M (1979) Reattachment flow issuing from a finite width nozzle. Bull JSME 22(165):340\u2013347. https:\/\/doi.org\/10.1299\/jsme1958.22.340","journal-title":"Bull JSME"},{"key":"841_CR14","doi-asserted-by":"publisher","first-page":"36","DOI":"10.1016\/j.compfluid.2013.02.007","volume":"77","author":"S Pramanik","year":"2013","unstructured":"Pramanik S, Das MK (2013) Numerical characterization of a planar turbulent offset jet over an oblique wall. Comput Fluids 77:36\u201355. https:\/\/doi.org\/10.1016\/j.compfluid.2013.02.007","journal-title":"Comput Fluids"},{"issue":"4","key":"841_CR15","doi-asserted-by":"publisher","first-page":"543","DOI":"10.1017\/S0022112060001304","volume":"9","author":"RA Sawyer","year":"1960","unstructured":"Sawyer RA (1960) The flow due to a two-dimensional jet issuing parallel to a flat plate. J Fluid Mech 9(4):543\u2013559. https:\/\/doi.org\/10.1017\/S0022112060001304","journal-title":"J Fluid Mech"},{"issue":"4","key":"841_CR16","doi-asserted-by":"publisher","first-page":"481","DOI":"10.1017\/S0022112063001464","volume":"17","author":"RA Sawyer","year":"1963","unstructured":"Sawyer RA (1963) Two-dimensional reattaching jet flows including the effects of curvature on entrainment. J Fluid Mech 17(4):481\u2013498. https:\/\/doi.org\/10.1017\/S0022112063001464","journal-title":"J Fluid Mech"},{"issue":"9","key":"841_CR17","doi-asserted-by":"publisher","DOI":"10.1115\/1.4043611","volume":"141","author":"JW Shi","year":"2019","unstructured":"Shi JW, Wang ZX, Zhou L, Zhang XB (2019) Numerical investigation on a new concept of shock vector control nozzle. J Eng Gas Turb Power 141(9):091004. https:\/\/doi.org\/10.1115\/1.4043611","journal-title":"J Eng Gas Turb Power"},{"issue":"13","key":"841_CR18","doi-asserted-by":"publisher","first-page":"2395","DOI":"10.1016\/S0017-9310(99)00312-9","volume":"43","author":"HB Song","year":"2000","unstructured":"Song HB, Yoon SH, Lee DH (2000) Flow and heat transfer characteristics of a two-dimensional oblique wall attaching offset jet. Int J Heat Mass Transf 43(13):2395\u20132404. https:\/\/doi.org\/10.1016\/S0017-9310(99)00312-9","journal-title":"Int J Heat Mass Transf"},{"issue":"10","key":"841_CR19","doi-asserted-by":"publisher","first-page":"2355","DOI":"10.2514\/1.J052971","volume":"52","author":"MJ Song","year":"2014","unstructured":"Song MJ, Park SH, Lee Y (2014) Application of backstep Coanda flap for supersonic coflowing fluidic thrust-vector control. AIAA J 52(10):2355\u20132359. https:\/\/doi.org\/10.2514\/1.J052971","journal-title":"AIAA J"},{"key":"841_CR20","doi-asserted-by":"publisher","DOI":"10.2514\/6.1992-3262","author":"PJ Strykowski","year":"1992","unstructured":"Strykowski PJ, Krothapalli A, Wishart D (1992) The enhancement of mixing in high-speed heated jets using a counter-flowing nozzle. AIAA. https:\/\/doi.org\/10.2514\/6.1992-3262","journal-title":"AIAA"},{"issue":"3","key":"841_CR21","doi-asserted-by":"publisher","first-page":"177","DOI":"10.1016\/j.ast.2018.11.059","volume":"86","author":"YS Wang","year":"2019","unstructured":"Wang YS, Xu JL, Huang S, Lin YC, Jiang JJ (2019) Computational study of axisymmetric divergent bypass dual throat nozzle. Aerosp Sci Technol 86(3):177\u2013190. https:\/\/doi.org\/10.1016\/j.ast.2018.11.059","journal-title":"Aerosp Sci Technol"},{"issue":"3","key":"841_CR22","doi-asserted-by":"publisher","first-page":"563","DOI":"10.1177\/0954410019872089","volume":"234","author":"YS Wang","year":"2020","unstructured":"Wang YS, Xu JL, Huang S, Lin YC, Jiang JJ (2020a) Experimental and numerical investigation of an axisymmetric divergent dual throat nozzle. Proc Inst Mech Eng Part G J Aerosp Eng 234(3):563\u2013572. https:\/\/doi.org\/10.1177\/0954410019872089","journal-title":"Proc Inst Mech Eng Part G J Aerosp Eng"},{"issue":"6","key":"841_CR23","doi-asserted-by":"publisher","DOI":"10.1115\/1.4045996","volume":"142","author":"YS Wang","year":"2020","unstructured":"Wang YS, Xu JL, Huang S, Jiang JJ, Pan RF (2020b) Design and preliminary analysis of the variable axisymmetric divergent bypass dual throat nozzle. J Fluids Eng 142(6):061204. https:\/\/doi.org\/10.1115\/1.4045996","journal-title":"J Fluids Eng"},{"key":"841_CR24","unstructured":"Wing DJ (1994) Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle. NASA TM-4574"},{"issue":"4","key":"841_CR25","doi-asserted-by":"publisher","first-page":"1412","DOI":"10.1177\/0954410017752580","volume":"233","author":"KX Wu","year":"2018","unstructured":"Wu KX, Kim HD, Jin Y (2018) Fluidic thrust vector control based on counter-flow concept. Proc Inst Mech Eng Part G J Aerosp Eng 233(4):1412\u20131422. https:\/\/doi.org\/10.1177\/0954410017752580","journal-title":"Proc Inst Mech Eng Part G J Aerosp Eng"},{"issue":"1","key":"841_CR26","doi-asserted-by":"publisher","first-page":"73","DOI":"10.47176\/jafm.14.01.31690","volume":"14","author":"KX Wu","year":"2021","unstructured":"Wu KX, Kim TH, Kim HD (2021) Numerical study of fluidic thrust vector control using dual throat nozzle. J Appl Fluid Mech 14(1):73\u201387. https:\/\/doi.org\/10.47176\/jafm.14.01.31690","journal-title":"J Appl Fluid Mech"},{"issue":"1","key":"841_CR27","doi-asserted-by":"publisher","first-page":"04020107","DOI":"10.1061\/(ASCE)AS.1943-5525.0001228","volume":"34","author":"KX Wu","year":"2021","unstructured":"Wu KX, Kim TH, Kim HD (2021b) Sensitivity analysis of counterflow thrust vector control with a three-dimensional rectangular nozzle. J Aerosp Eng 34(1):04020107. https:\/\/doi.org\/10.1061\/(ASCE)AS.1943-5525.0001228","journal-title":"J Aerosp Eng"},{"issue":"11","key":"841_CR28","first-page":"1967","volume":"33","author":"ZY Xiao","year":"2012","unstructured":"Xiao ZY, Gu YS, Jiang X, Chen ZB (2012) A new fluidic thrust vectoring technique based on ejecting mixing effects. Acta Aeronaut Astronaut Sin 33(11):1967\u20131974","journal-title":"Acta Aeronaut Astronaut Sin"}],"container-title":["Journal of Visualization"],"original-title":[],"language":"en","link":[{"URL":"https:\/\/link.springer.com\/content\/pdf\/10.1007\/s12650-022-00841-y.pdf","content-type":"application\/pdf","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/link.springer.com\/article\/10.1007\/s12650-022-00841-y\/fulltext.html","content-type":"text\/html","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/link.springer.com\/content\/pdf\/10.1007\/s12650-022-00841-y.pdf","content-type":"application\/pdf","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2022,8,31]],"date-time":"2022-08-31T14:26:02Z","timestamp":1661955962000},"score":1,"resource":{"primary":{"URL":"https:\/\/link.springer.com\/10.1007\/s12650-022-00841-y"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2022,5,10]]},"references-count":28,"journal-issue":{"issue":"5","published-print":{"date-parts":[[2022,10]]}},"alternative-id":["841"],"URL":"https:\/\/doi.org\/10.1007\/s12650-022-00841-y","relation":{},"ISSN":["1343-8875","1875-8975"],"issn-type":[{"type":"print","value":"1343-8875"},{"type":"electronic","value":"1875-8975"}],"subject":[],"published":{"date-parts":[[2022,5,10]]},"assertion":[{"value":"30 October 2021","order":1,"name":"received","label":"Received","group":{"name":"ArticleHistory","label":"Article History"}},{"value":"28 December 2021","order":2,"name":"revised","label":"Revised","group":{"name":"ArticleHistory","label":"Article History"}},{"value":"1 April 2022","order":3,"name":"accepted","label":"Accepted","group":{"name":"ArticleHistory","label":"Article History"}},{"value":"10 May 2022","order":4,"name":"first_online","label":"First Online","group":{"name":"ArticleHistory","label":"Article History"}}]}}