{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,2,21]],"date-time":"2025-02-21T17:14:29Z","timestamp":1740158069708,"version":"3.37.3"},"reference-count":75,"publisher":"Springer Science and Business Media LLC","issue":"6","license":[{"start":{"date-parts":[[2023,6,26]],"date-time":"2023-06-26T00:00:00Z","timestamp":1687737600000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/www.springernature.com\/gp\/researchers\/text-and-data-mining"},{"start":{"date-parts":[[2023,6,26]],"date-time":"2023-06-26T00:00:00Z","timestamp":1687737600000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/www.springernature.com\/gp\/researchers\/text-and-data-mining"}],"funder":[{"name":"Science and Engineering Research Board, Department of Science and Technology","award":["CRG\/2018\/003925"],"award-info":[{"award-number":["CRG\/2018\/003925"]}]}],"content-domain":{"domain":["link.springer.com"],"crossmark-restriction":false},"short-container-title":["J Vis"],"published-print":{"date-parts":[[2023,12]]},"DOI":"10.1007\/s12650-023-00933-3","type":"journal-article","created":{"date-parts":[[2023,6,26]],"date-time":"2023-06-26T21:01:54Z","timestamp":1687813314000},"page":"1279-1297","update-policy":"https:\/\/doi.org\/10.1007\/springer_crossmark_policy","source":"Crossref","is-referenced-by-count":2,"title":["Mitigation of shock-induced flow separation over an axisymmetric flared body using ramped vanes"],"prefix":"10.1007","volume":"26","author":[{"ORCID":"https:\/\/orcid.org\/0000-0002-0975-3506","authenticated-orcid":false,"given":"T.","family":"Nilavarasan","sequence":"first","affiliation":[]},{"given":"G. N.","family":"Joshi","sequence":"additional","affiliation":[]},{"given":"A.","family":"Misra","sequence":"additional","affiliation":[]},{"given":"C.","family":"Manisankar","sequence":"additional","affiliation":[]},{"given":"S. B.","family":"Verma","sequence":"additional","affiliation":[]}],"member":"297","published-online":{"date-parts":[[2023,6,26]]},"reference":[{"issue":"1","key":"933_CR1","doi-asserted-by":"publisher","first-page":"62","DOI":"10.2514\/1.46655","volume":"47","author":"MYM Ahmed","year":"2010","unstructured":"Ahmed MYM, Qin N (2010) Drag reduction using aerodisks for hypersonic hemispherical bodies. J Spacecr Rockets 47(1):62\u201380. https:\/\/doi.org\/10.2514\/1.46655","journal-title":"J Spacecr Rockets"},{"key":"933_CR2","doi-asserted-by":"publisher","DOI":"10.2514\/6.2006-3197","author":"BH Anderson","year":"2006","unstructured":"Anderson BH, Tinapple J, Surber L (2006) Optimal control of shock wave turbulent boundary layer interactions using micro-array actuation. AIAA Paper. https:\/\/doi.org\/10.2514\/6.2006-3197","journal-title":"AIAA Paper"},{"issue":"996","key":"933_CR3","doi-asserted-by":"publisher","first-page":"209","DOI":"10.1017\/S0001924000067166","volume":"100","author":"H Babinsky","year":"1996","unstructured":"Babinsky H, Edwards JA (1996) On the incipient separation of a turbulent hypersonic boundary layer. Aeronaut J 100(996):209\u2013214. https:\/\/doi.org\/10.1017\/S0001924000067166","journal-title":"Aeronaut J"},{"issue":"3","key":"933_CR4","doi-asserted-by":"publisher","first-page":"668","DOI":"10.2514\/1.38022","volume":"47","author":"H Babinsky","year":"2009","unstructured":"Babinsky H, Li Y, Pitt Ford CW (2009) Microramp control of oblique shock-wave\/boundary-layer interactions. AIAA J 47(3):668\u2013675. https:\/\/doi.org\/10.2514\/1.38022","journal-title":"AIAA J"},{"key":"933_CR5","unstructured":"Blevins RD, Bofilios D, Holehouse I, Hwa VW, Tratt, MD, Laganelli AL, Pozefsky P and Pierucci P (2009) Thermo-Vibro-Acoustic loads and fatigue of hypersonic flight vehicle structure. AFRL-RB-WP-TR-2009-3139."},{"key":"933_CR6","unstructured":"Bross M, Scharnowski S and Kahler CJ (2018) Influence of leading edge tripping devices on supersonic boundary layer characteristics. In: 5th International conference on experimental fluid mechanics, Munich, Germany"},{"key":"933_CR7","unstructured":"Cole HA, Erickson AL and Rainey AG (1970) Buffeting during atmospheric ascent. NASA SP-8001."},{"issue":"1","key":"933_CR8","doi-asserted-by":"publisher","first-page":"119","DOI":"10.2514\/3.49175","volume":"12","author":"GT Coleman","year":"1973","unstructured":"Coleman GT, Stollery JL (1973) Incipient separation of axially symmetric hypersonic turbulent boundary layers. AIAA J 12(1):119\u2013120. https:\/\/doi.org\/10.2514\/3.49175","journal-title":"AIAA J"},{"key":"933_CR9","doi-asserted-by":"publisher","DOI":"10.2514\/6.2015-0314","author":"JR DeBonis","year":"2015","unstructured":"DeBonis JR (2015) Evaluation of industry standard turbulence models on an axisymmetric supersonic compression corner. AIAA Paper. https:\/\/doi.org\/10.2514\/6.2015-0314","journal-title":"AIAA Paper"},{"key":"933_CR10","doi-asserted-by":"publisher","DOI":"10.1002\/9781118578544","volume-title":"Three-dimensional separated flow topology: Critical points, separation lines and vortical structres","author":"JM Delery","year":"2013","unstructured":"Delery JM (2013) Three-dimensional separated flow topology: Critical points, separation lines and vortical structres. John Wiley and Sons Inc, USA"},{"issue":"8","key":"933_CR11","doi-asserted-by":"publisher","first-page":"1517","DOI":"10.2514\/2.1476","volume":"39","author":"DS Dolling","year":"2001","unstructured":"Dolling DS (2001) Fifty years of shock-wave\/boundary-layer interaction research: What next? AIAA J 39(8):1517\u20131531. https:\/\/doi.org\/10.2514\/2.1476","journal-title":"AIAA J"},{"issue":"6","key":"933_CR12","doi-asserted-by":"publisher","first-page":"734","DOI":"10.2514\/3.10173","volume":"27","author":"DS Dolling","year":"1989","unstructured":"Dolling DS, Brusniak L (1989) Separation shock motion in fin, cylinder and compression ramp - induced turbulent interactions. AIAA J 27(6):734\u2013742. https:\/\/doi.org\/10.2514\/3.10173","journal-title":"AIAA J"},{"key":"933_CR13","doi-asserted-by":"crossref","unstructured":"Edney B (1968) Anomalous heat transfer and pressure distributions on blunt bodies at hypersonic speeds in the presence of impinging shock. FFA Report, Aeronautical Research Institute of Sweden.","DOI":"10.2172\/4480948"},{"issue":"5","key":"933_CR14","doi-asserted-by":"publisher","first-page":"728","DOI":"10.2514\/3.60176","volume":"29","author":"ME Erengil","year":"1993","unstructured":"Erengil ME, Dolling DS (1993) Effect of sweepback on unsteady separation in Mach 5 compression ramp interactions. AIAA J 29(5):728\u2013735. https:\/\/doi.org\/10.2514\/3.60176","journal-title":"AIAA J"},{"issue":"4","key":"933_CR15","doi-asserted-by":"publisher","first-page":"481","DOI":"10.2514\/3.28216","volume":"2","author":"LE Ericcson","year":"1965","unstructured":"Ericcson LE, Reding JP (1965) Analysis of flow separation effects on the dynamics of a large space booster. J Spacecr Rockets 2(4):481\u2013490. https:\/\/doi.org\/10.2514\/3.28216","journal-title":"J Spacecr Rockets"},{"issue":"5","key":"933_CR16","doi-asserted-by":"publisher","first-page":"521","DOI":"10.1007\/s00193-014-0514-7","volume":"25","author":"D Estruch-samper","year":"2015","unstructured":"Estruch-samper D, Vanstone L, Hillier R, Ganapathisubramani B (2015) Micro vortex generator control of axisymmetric high-speed laminar boundary layer separation. Shock Waves 25(5):521\u2013533. https:\/\/doi.org\/10.1007\/s00193-014-0514-7","journal-title":"Shock Waves"},{"issue":"2","key":"933_CR17","doi-asserted-by":"publisher","first-page":"151","DOI":"10.2514\/3.58756","volume":"14","author":"MK Fukuda","year":"1977","unstructured":"Fukuda MK, Hingst WR, Reshotko E (1977) Bleed effects on Shock\/Boundary-layer interactionsin supersonic mixed compression inlets. J Aircraft 14(2):151\u2013156. https:\/\/doi.org\/10.2514\/3.58756","journal-title":"J Aircraft"},{"issue":"8","key":"933_CR18","doi-asserted-by":"publisher","first-page":"3379","DOI":"10.2514\/1.J057846","volume":"57","author":"ML Funderburk","year":"2019","unstructured":"Funderburk ML, Narayanaswamy V (2019) Experimental investigation of microramp control of an axisymmetric shock\/boundary-layer interaction. AIAA J 57(8):3379\u20133394. https:\/\/doi.org\/10.2514\/1.J057846","journal-title":"AIAA J"},{"key":"933_CR19","doi-asserted-by":"publisher","first-page":"066101","DOI":"10.1063\/1.4881941","volume":"26","author":"RHM Geipmann","year":"2014","unstructured":"Geipmann RHM, Schrijer FFJ, van Oudheusden BW (2014) Flow control of an oblique shock wave reflection with micro-ramp vortex generators: effect of location and size. Phys Fluids 26:066101. https:\/\/doi.org\/10.1063\/1.4881941","journal-title":"Phys Fluids"},{"key":"933_CR20","doi-asserted-by":"publisher","DOI":"10.2514\/6.2018-0158","author":"R Gejji","year":"2018","unstructured":"Gejji R, Walters I, Beard S, Lemcherfi A, Sardeshmukh S, Heister S, Slabaugh C (2018) Transducer installation effects on pressure measurements in pressure gain combustion devices. AIAA Paper. https:\/\/doi.org\/10.2514\/6.2018-0158","journal-title":"AIAA Paper"},{"issue":"4","key":"933_CR21","doi-asserted-by":"publisher","first-page":"759","DOI":"10.2514\/3.6271","volume":"9","author":"JJ Ginoux","year":"1971","unstructured":"Ginoux JJ (1971) Streamwise vortices in reattaching high-speed flows: a suggested approach. AIAA J 9(4):759\u2013760. https:\/\/doi.org\/10.2514\/3.6271","journal-title":"AIAA J"},{"issue":"6","key":"933_CR22","doi-asserted-by":"publisher","first-page":"561","DOI":"10.1016\/0045-7930(96)00019-9","volume":"25","author":"F Grasso","year":"1996","unstructured":"Grasso F, Marini M (1996) Analysis of hypersonic shock-wave laminar boundary-layer interaction phenomena. Comput Fluids 25(6):561\u2013581. https:\/\/doi.org\/10.1016\/0045-7930(96)00019-9","journal-title":"Comput Fluids"},{"key":"933_CR23","doi-asserted-by":"publisher","DOI":"10.2514\/6.1993-3131","author":"KS Heffner","year":"1993","unstructured":"Heffner KS, Chpoun A, Lengrands JC (1993) Experimental study of transitional axisymmetric shock\u2014boundary layer interactions at Mach 5. AIAA Paper. https:\/\/doi.org\/10.2514\/6.1993-3131","journal-title":"AIAA Paper"},{"issue":"11","key":"933_CR24","doi-asserted-by":"publisher","first-page":"2529","DOI":"10.2514\/1.J050313","volume":"48","author":"T Herges","year":"2010","unstructured":"Herges T, Kroeker L, Elliot G, Dutton C (2010) Microramp flow control of normal shock\/boundary layer interactions. AIAA J 48(11):2529\u20132542. https:\/\/doi.org\/10.2514\/1.J050313","journal-title":"AIAA J"},{"key":"933_CR25","doi-asserted-by":"publisher","first-page":"056102","DOI":"10.1063\/5.0005431","volume":"32","author":"W Hu","year":"2020","unstructured":"Hu W, Hickel S, van Oudheusden B (2020) Influence of the upstream disturbances on the primary and secondary instabilities in a supersonic separated flow over a backward facing step. Phys Fluids 32:056102. https:\/\/doi.org\/10.1063\/5.0005431","journal-title":"Phys Fluids"},{"key":"933_CR26","doi-asserted-by":"publisher","first-page":"103","DOI":"10.1016\/j.actaastro.2020.05.001","volume":"174","author":"W Huang","year":"2020","unstructured":"Huang W, Wu H, Yang Y, Yan L, Li S (2020) Recent advances in the shock wave\/boundary layer interaction and its control in internal and external flows. Acta Astronaut 174:103\u2013122. https:\/\/doi.org\/10.1016\/j.actaastro.2020.05.001","journal-title":"Acta Astronaut"},{"issue":"3","key":"933_CR27","doi-asserted-by":"publisher","first-page":"543","DOI":"10.1121\/1.19118998","volume":"36","author":"AL Kistler","year":"1964","unstructured":"Kistler AL (1964) Fluctuating wall pressure under a separated supersonic flow. J Acoust Soc Am 36(3):543\u2013550. https:\/\/doi.org\/10.1121\/1.19118998","journal-title":"J Acoust Soc Am"},{"issue":"1027","key":"933_CR28","doi-asserted-by":"publisher","first-page":"209","DOI":"10.1017\/S0001924000027950","volume":"103","author":"K Kontis","year":"1999","unstructured":"Kontis K, Stollery JL (1999) Incipient separation on flared bodies at hypersonic speeds. Aeronaut J 103(1027):209\u2013214. https:\/\/doi.org\/10.1017\/S0001924000027950","journal-title":"Aeronaut J"},{"issue":"5","key":"933_CR29","doi-asserted-by":"publisher","first-page":"771","DOI":"10.2514\/3.6275","volume":"9","author":"RH Korkegi","year":"1971","unstructured":"Korkegi RH (1971) Survey of viscous interactions associated with high Mach number flight. AIAA J 9(5):771\u2013784. https:\/\/doi.org\/10.2514\/3.6275","journal-title":"AIAA J"},{"key":"933_CR30","unstructured":"Kuehn DM (1961) Turbulent boundary layer separation induced by flares on cylinders at zero angle of attack. Technical report R-117."},{"key":"933_CR31","unstructured":"Lambourne NC (1962) Control surface buzz. Technical Report, Ministry of Aviation, Aeronautical Research Council, London."},{"issue":"1149","key":"933_CR32","doi-asserted-by":"publisher","first-page":"683","DOI":"10.1017\/s0001924000003353","volume":"113","author":"S Lee","year":"2009","unstructured":"Lee S, Loth E (2009) Supersonic boundary\u2014layer interactions with various micro-vortex generator geometries. Aeronaut J 113(1149):683\u2013697. https:\/\/doi.org\/10.1017\/s0001924000003353","journal-title":"Aeronaut J"},{"issue":"1256","key":"933_CR33","doi-asserted-by":"publisher","first-page":"1568","DOI":"10.1017\/aer.2018.88","volume":"122","author":"S Lee","year":"2018","unstructured":"Lee S, Loth E (2018) On ramped vanes to control normal shock boundary layer interactions. Aeronaut J 122(1256):1568\u20131585. https:\/\/doi.org\/10.1017\/aer.2018.88","journal-title":"Aeronaut J"},{"key":"933_CR34","doi-asserted-by":"publisher","first-page":"233","DOI":"10.1016\/j.compfluid.2011.06.003","volume":"49","author":"S Lee","year":"2011","unstructured":"Lee S, Loth E, Babinsky H (2011) Normal shock boundary layer control with various micro vortex generator geometries. Comput Fluids 49:233\u2013246. https:\/\/doi.org\/10.1016\/j.compfluid.2011.06.003","journal-title":"Comput Fluids"},{"key":"933_CR35","unstructured":"Lighthill JM (1963) Attachment and separation in three dimensional flow. In: Rosenhead (Ed) Laminar boundary-layer theory, Oxford University Press, Oxford, pp 77\u201382"},{"issue":"1","key":"933_CR36","doi-asserted-by":"publisher","first-page":"23","DOI":"10.1006\/jcph.1993.1122","volume":"107","author":"MS Liou","year":"1993","unstructured":"Liou MS, Steffen C (1993) A new flux splitting scheme. J Comput Phys 107(1):23\u201339. https:\/\/doi.org\/10.1006\/jcph.1993.1122","journal-title":"J Comput Phys"},{"issue":"5","key":"933_CR37","doi-asserted-by":"publisher","first-page":"747","DOI":"10.1007\/s00193-016-0690-8","volume":"27","author":"RR Martis","year":"2017","unstructured":"Martis RR, Misra A (2017) Separation attenuation in swept shock wave\u2014boundary-layer interaction using different micro vortex generator geometries. Shock Waves 27(5):747\u2013760. https:\/\/doi.org\/10.1007\/s00193-016-0690-8","journal-title":"Shock Waves"},{"issue":"3","key":"933_CR38","doi-asserted-by":"publisher","first-page":"591","DOI":"10.2514\/1.J052470","volume":"52","author":"RR Martis","year":"2014","unstructured":"Martis RR, Misra A, Singh A (2014) Effect of microramps on swept shock wave\u2014boundary layer interaction. AIAA J 52(3):591\u2013603. https:\/\/doi.org\/10.2514\/1.J052470","journal-title":"AIAA J"},{"key":"933_CR39","doi-asserted-by":"publisher","first-page":"584","DOI":"10.1017\/S0022112060000815","volume":"4","author":"DJ Maull","year":"1960","unstructured":"Maull DJ (1960) Hypersonic flow over axially symmetric spiked bodies. J Fluid Mech 4:584\u2013592. https:\/\/doi.org\/10.1017\/S0022112060000815","journal-title":"J Fluid Mech"},{"key":"933_CR40","doi-asserted-by":"publisher","DOI":"10.2514\/6.1992-64","author":"DC McCormick","year":"1992","unstructured":"McCormick DC (1992) Shock\u2014boundary layer interaction control with low-profile vortex generators and passive cavity. AIAA Paper. https:\/\/doi.org\/10.2514\/6.1992-64","journal-title":"AIAA Paper"},{"issue":"2","key":"933_CR41","doi-asserted-by":"publisher","first-page":"297","DOI":"10.2514\/1.41352","volume":"48","author":"V Narayanaswamy","year":"2010","unstructured":"Narayanaswamy V, Raja LL, Clemens NT (2010) Characterization of a high-frequency pulsed-plasma jet actuator for supersonic flow control. AIAA J 48(2):297\u2013305. https:\/\/doi.org\/10.2514\/1.41352","journal-title":"AIAA J"},{"key":"933_CR42","doi-asserted-by":"publisher","first-page":"225","DOI":"10.1016\/j.compfluid.2004.05.002","volume":"34","author":"S Navarro-Martinez","year":"2005","unstructured":"Navarro-Martinez S, Tutty OR (2005) Numerical simulations of Gortler vortices in hypersonic compression ramps. Comput Fluids 34:225\u2013247. https:\/\/doi.org\/10.1016\/j.compfluid.2004.05.002","journal-title":"Comput Fluids"},{"key":"933_CR43","unstructured":"Nilavarasan T (2022) Flare-induced Shock Wave-Boundary Layer Interaction and its control using Micro Vortex Generators. Ph.D Thesis, Defence Institute of Advanced Technology, Pune, India"},{"key":"933_CR44","doi-asserted-by":"publisher","first-page":"489","DOI":"10.1007\/978-981-19-6970-6_78","volume-title":"Fluid Mechanics and Fluid Power. Lecture Notes in Mechanical Engineering","author":"T Nilavarasan","year":"2023","unstructured":"Nilavarasan T, Joshi GN (2023) Attenuation of compression ramp-induced flow separation using ramped vanes. In: Bhattacharyya S, Benim AC (eds) Fluid Mechanics and Fluid Power. Lecture Notes in Mechanical Engineering, vol 2. Springer, pp 489\u2013494. https:\/\/doi.org\/10.1007\/978-981-19-6970-6_78"},{"issue":"1271","key":"933_CR45","doi-asserted-by":"publisher","first-page":"121","DOI":"10.1017\/aer.2019.138","volume":"124","author":"T Nilavarasan","year":"2020","unstructured":"Nilavarasan T, Joshi GN, Misra A (2020) Effect of microramps on flare-induced shock\u2014boundary-layer interaction. Aeronaut J 124(1271):121\u2013149. https:\/\/doi.org\/10.1017\/aer.2019.138","journal-title":"Aeronaut J"},{"issue":"5","key":"933_CR46","doi-asserted-by":"publisher","first-page":"991","DOI":"10.1007\/s12650-020-00735-x","volume":"24","author":"T Nilavarasan","year":"2021","unstructured":"Nilavarasan T, Joshi GN, Misra A, Manisankar C, Verma SB (2021) Topological modifications due to ramped vanes in a flare-induced shock\u2014boundary layer interaction flowfield. J vis 24(5):991\u20131010. https:\/\/doi.org\/10.1007\/s12650-020-00735-x","journal-title":"J vis"},{"key":"933_CR47","doi-asserted-by":"publisher","first-page":"160","DOI":"10.1016\/j.euromechflu.2022.04.010","volume":"95","author":"T Nilavarasan","year":"2022","unstructured":"Nilavarasan T, Joshi GN, Misra A, Manisankar C, Verma SB (2022) Control of flow separation over an axisymmetric flared body using ramped vanes. Euro J Mech B\/fluids 95:160\u2013177. https:\/\/doi.org\/10.1016\/j.euromechflu.2022.04.010","journal-title":"Euro J Mech B\/fluids"},{"issue":"8","key":"933_CR48","doi-asserted-by":"publisher","first-page":"1890","DOI":"10.1177\/09544100221139958","volume":"237","author":"T Nilavarasan","year":"2023","unstructured":"Nilavarasan T, Joshi GN, Misra A, Manisankar C, Verma SB (2023a) Performance evaluation of different micro vortex generators in controlling a flare-induced shock\u2014boundary layer interaction. Proc Inst Mech Eng Part G: J Aerospace Eng 237(8):1890\u20131915. https:\/\/doi.org\/10.1177\/09544100221139958","journal-title":"Proc Inst Mech Eng Part G: J Aerospace Eng"},{"key":"933_CR49","doi-asserted-by":"publisher","first-page":"98","DOI":"10.1016\/j.euromechflu.2023.01.007","volume":"99","author":"T Nilavarasan","year":"2023","unstructured":"Nilavarasan T, Joshi GN, Misra A, Manisankar C, Verma SB (2023b) Spatial and temporal alterations due to vortex generators on a flare-induced shock-boundary layer interaction. Euro J Mech B\/fluids 99:98\u2013115. https:\/\/doi.org\/10.1016\/j.euromechflu.2023.01.007","journal-title":"Euro J Mech B\/fluids"},{"key":"933_CR50","doi-asserted-by":"publisher","first-page":"71","DOI":"10.2514\/6.2011-71","volume":"2011","author":"WR Nolan","year":"2011","unstructured":"Nolan WR, Babinsky H (2011) Characterization of micro-vortex generators in supersonic flows. AIAA Paper 2011:71. https:\/\/doi.org\/10.2514\/6.2011-71","journal-title":"AIAA Paper"},{"key":"933_CR51","doi-asserted-by":"publisher","first-page":"16","DOI":"10.1016\/j.paerosci.2014.12.006","volume":"74","author":"AG Panaras","year":"2015","unstructured":"Panaras AG, Lu FK (2015) Micro Vortex Generators for shock wave\/boundary layer interactions. Prog Aero Sci 74:16\u201347. https:\/\/doi.org\/10.1016\/j.paerosci.2014.12.006","journal-title":"Prog Aero Sci"},{"issue":"7","key":"933_CR52","doi-asserted-by":"publisher","first-page":"816","DOI":"10.2514\/3.9974","volume":"26","author":"WR Pauley","year":"1988","unstructured":"Pauley WR, Eaton JK (1988) Experimental study of the development of longitudinal vortex pairs embedded in a turbulent boundary layer. AIAA J 26(7):816\u2013823. https:\/\/doi.org\/10.2514\/3.9974","journal-title":"AIAA J"},{"key":"933_CR53","doi-asserted-by":"publisher","DOI":"10.2514\/6.1993-401","author":"RJ Pegg","year":"1993","unstructured":"Pegg RJ, Hunt JL, Petley DH, Burkardt L, Stevens DR, Moses PL, Pinckney SZ, Kabis HZ, Spoth KA, Dziedzic WM, Kries RI, Marti JG (1993) Design of a hypersonic wave-rider derived airplane. AIAA Paper. https:\/\/doi.org\/10.2514\/6.1993-401","journal-title":"AIAA Paper"},{"issue":"11","key":"933_CR54","doi-asserted-by":"publisher","first-page":"4794","DOI":"10.2514\/1.J059624","volume":"58","author":"JD Pickles","year":"2020","unstructured":"Pickles JD, Narayanswamy V (2020) Control of fin shock induced flow separation using vortex generators. AIAA J 58(11):4794\u20134806. https:\/\/doi.org\/10.2514\/1.J059624","journal-title":"AIAA J"},{"key":"933_CR55","doi-asserted-by":"publisher","first-page":"1","DOI":"10.1017\/jfm.2011.560","volume":"699","author":"S Priebe","year":"2012","unstructured":"Priebe S, Martin MP (2012) Low-frequency unsteadiness in shock wave-turbulent boundary layer interaction. J Fluid Mech 699:1\u201349. https:\/\/doi.org\/10.1017\/jfm.2011.560","journal-title":"J Fluid Mech"},{"key":"933_CR56","doi-asserted-by":"crossref","unstructured":"Raman KR (1974) A study of surface pressure fluctuations in hypersonic turbulent boundary layers. NASA CR-2386","DOI":"10.2514\/6.1973-997"},{"issue":"3","key":"933_CR57","doi-asserted-by":"publisher","first-page":"927","DOI":"10.2514\/1.J059674","volume":"59","author":"DP Ramaswamy","year":"2021","unstructured":"Ramaswamy DP, Schreyer A-M (2021) Control of shock-induced separation of a turbulent boundary layer using air-jet vortex generators. AIAA J 59(3):927\u2013939. https:\/\/doi.org\/10.2514\/1.J059674","journal-title":"AIAA J"},{"key":"933_CR58","doi-asserted-by":"publisher","first-page":"139","DOI":"10.1007\/s00348-017-2422-y","volume":"58","author":"A Roghelia","year":"2017","unstructured":"Roghelia A, Olivier H, Egorov IV, Chuvakhov P (2017) Experimental investigation of Gortler vortices in hypersonic ramp flows. Exp Fluids 58:139. https:\/\/doi.org\/10.1007\/s00348-017-2422-y","journal-title":"Exp Fluids"},{"issue":"6","key":"933_CR59","doi-asserted-by":"publisher","first-page":"976","DOI":"10.2514\/3.3590","volume":"4","author":"A Roshko","year":"1966","unstructured":"Roshko A, Thomke GJ (1966) Observations of turbulent reattachment behind an axisymmetric downstream-facing step iin supersonic flow. AIAA J 4(6):976\u2013980. https:\/\/doi.org\/10.2514\/3.3590","journal-title":"AIAA J"},{"issue":"7","key":"933_CR60","doi-asserted-by":"publisher","first-page":"873","DOI":"10.2514\/3.61429","volume":"14","author":"A Roshko","year":"1976","unstructured":"Roshko A, Thomke GJ (1976) Flare induced interaction lengths in supersonic turbulent boundary layers. AIAA J 14(7):873\u2013879. https:\/\/doi.org\/10.2514\/3.61429","journal-title":"AIAA J"},{"key":"933_CR61","doi-asserted-by":"publisher","first-page":"109911","DOI":"10.1016\/j.expthermflusci.2019.109911","volume":"109","author":"CL Running","year":"2019","unstructured":"Running CL, Juliano TJ, Jewell JS, Borg MP, Kimmel RL (2019) Hypersonic shock-wave\/boundary-layer interactions on a cone\/flare. Exp Therm Fluid Sci 109:109911. https:\/\/doi.org\/10.1016\/j.expthermflusci.2019.109911","journal-title":"Exp Therm Fluid Sci"},{"key":"933_CR62","doi-asserted-by":"publisher","DOI":"10.2514\/6.2020-2961","author":"S Sajeev","year":"2020","unstructured":"Sajeev S, Sandhu JPS, Ghosh S, Edwards JR (2020) Effectiveness of micro-vortex generators in tandem in high speed flows. AIAA Paper. https:\/\/doi.org\/10.2514\/6.2020-2961","journal-title":"AIAA Paper"},{"key":"933_CR63","doi-asserted-by":"publisher","DOI":"10.2514\/6.1992-439","author":"PR Spalart","year":"1992","unstructured":"Spalart PR, Allmaras SR (1992) A one-equation turbulence model for aerodynamic flows. AIAA Paper. https:\/\/doi.org\/10.2514\/6.1992-439","journal-title":"AIAA Paper"},{"issue":"838","key":"933_CR64","doi-asserted-by":"publisher","first-page":"278","DOI":"10.1098\/rspa.1933.0018","volume":"139","author":"GI Taylor","year":"1933","unstructured":"Taylor GI, Macoll JW (1933) The air pressure on a cone moving at high speeds\u2014I. Proc R Soc Lond Ser A 139(838):278\u2013297. https:\/\/doi.org\/10.1098\/rspa.1933.0018","journal-title":"Proc R Soc Lond Ser A"},{"key":"933_CR65","doi-asserted-by":"publisher","DOI":"10.2514\/6.2013-18","author":"N Titchener","year":"2013","unstructured":"Titchener N, Babinsky H (2013) The effects of various vortex generator configurations on a Normal shock wave\/boundary layer interaction. AIAA Paper. https:\/\/doi.org\/10.2514\/6.2013-18","journal-title":"AIAA Paper"},{"issue":"5","key":"933_CR66","doi-asserted-by":"publisher","first-page":"473","DOI":"10.1007\/s00193-015-0551-x","volume":"25","author":"N Titchener","year":"2015","unstructured":"Titchener N, Babinsky H (2015) A review of the use of vortex generators for mitigating shock induced separation. Shock Waves 25(5):473\u2013494. https:\/\/doi.org\/10.1007\/s00193-015-0551-x","journal-title":"Shock Waves"},{"issue":"5","key":"933_CR67","doi-asserted-by":"publisher","first-page":"443","DOI":"10.1007\/s00191-015-0587-y","volume":"25","author":"SB Verma","year":"2015","unstructured":"Verma SB, Hadjadj A (2015) Supersonic flow control. Shock Waves 25(5):443\u2013449. https:\/\/doi.org\/10.1007\/s00191-015-0587-y","journal-title":"Shock Waves"},{"issue":"3","key":"933_CR68","doi-asserted-by":"publisher","first-page":"467","DOI":"10.2514\/2.3831","volume":"39","author":"SB Verma","year":"2002","unstructured":"Verma SB, Koppenwallner G (2002) Unsteady separation in flare-induced hypersonic shock-wave-boundary-layer interaction flowfield. J Spacecr Rockets 39(3):467\u2013470. https:\/\/doi.org\/10.2514\/2.3831","journal-title":"J Spacecr Rockets"},{"issue":"7","key":"933_CR69","doi-asserted-by":"publisher","first-page":"2228","DOI":"10.2514\/1.J055446","volume":"55","author":"SB Verma","year":"2017","unstructured":"Verma SB, Manisankar C (2017) Assessment of various low-profile mechanical vortex generators in controlling a shock\u2014induced separation. AIAA J 55(7):2228\u20132240. https:\/\/doi.org\/10.2514\/1.J055446","journal-title":"AIAA J"},{"issue":"4","key":"933_CR70","doi-asserted-by":"publisher","first-page":"1600","DOI":"10.2514\/1.J056460","volume":"56","author":"SB Verma","year":"2018","unstructured":"Verma SB, Manisankar C (2018) Control of incident shock\u2014induced separation using vane-type vortex generating devices. AIAA J 56(4):1600\u20131615. https:\/\/doi.org\/10.2514\/1.J056460","journal-title":"AIAA J"},{"issue":"7","key":"933_CR71","doi-asserted-by":"publisher","first-page":"2892","DOI":"10.2514\/1.J057509","volume":"57","author":"SB Verma","year":"2019","unstructured":"Verma SB, Manisankar C (2019) Control of compression corner induced interaction with steady microjets. AIAA J 57(7):2892\u20132904. https:\/\/doi.org\/10.2514\/1.J057509","journal-title":"AIAA J"},{"key":"933_CR72","doi-asserted-by":"publisher","first-page":"725","DOI":"10.1016\/j.ast.2017.10.014","volume":"71","author":"SB Verma","year":"2017","unstructured":"Verma SB, Hadjadj A, Haidn O (2017) Origin of side-loads in a subscale truncated ideal contour nozzle. Aero Sci Tech 71:725\u2013732. https:\/\/doi.org\/10.1016\/j.ast.2017.10.014","journal-title":"Aero Sci Tech"},{"issue":"6","key":"933_CR73","doi-asserted-by":"publisher","first-page":"1528","DOI":"10.2514\/1.40966","volume":"47","author":"JL Wagner","year":"2009","unstructured":"Wagner JL, Yuceil KB, Valdivia A, Clemens NT, Dolling DS (2009) Experimental investigation of unstart in an inlet\/isolator model in Mach 5 flow. AIAA J 47(6):1528\u20131542. https:\/\/doi.org\/10.2514\/1.40966","journal-title":"AIAA J"},{"key":"933_CR74","doi-asserted-by":"publisher","DOI":"10.2514\/6.1974-1063","author":"WF Wong","year":"1974","unstructured":"Wong WF (1974) The application of boundary layer suction to suppress strong shock-induced separation in supersonic inlets. AIAA Paper. https:\/\/doi.org\/10.2514\/6.1974-1063","journal-title":"AIAA Paper"},{"key":"933_CR75","doi-asserted-by":"publisher","DOI":"10.1017\/CBO9780511842727.005","volume-title":"Shock wave\u2014boundary layer interactions","author":"AA Zheltovodov","year":"2011","unstructured":"Zheltovodov AA, Knight DD (2011) Ideal-gas shock-wave turbulent boundary-layer interactions in supersonic flows and their modelling: three-dimensional interactions. In: Babinsky H, Harvey JK (eds) Shock wave\u2014boundary layer interactions. Cambridge University Press, UK. https:\/\/doi.org\/10.1017\/CBO9780511842727.005"}],"container-title":["Journal of Visualization"],"original-title":[],"language":"en","link":[{"URL":"https:\/\/link.springer.com\/content\/pdf\/10.1007\/s12650-023-00933-3.pdf","content-type":"application\/pdf","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/link.springer.com\/article\/10.1007\/s12650-023-00933-3\/fulltext.html","content-type":"text\/html","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/link.springer.com\/content\/pdf\/10.1007\/s12650-023-00933-3.pdf","content-type":"application\/pdf","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2023,10,13]],"date-time":"2023-10-13T05:17:47Z","timestamp":1697174267000},"score":1,"resource":{"primary":{"URL":"https:\/\/link.springer.com\/10.1007\/s12650-023-00933-3"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2023,6,26]]},"references-count":75,"journal-issue":{"issue":"6","published-print":{"date-parts":[[2023,12]]}},"alternative-id":["933"],"URL":"https:\/\/doi.org\/10.1007\/s12650-023-00933-3","relation":{},"ISSN":["1343-8875","1875-8975"],"issn-type":[{"type":"print","value":"1343-8875"},{"type":"electronic","value":"1875-8975"}],"subject":[],"published":{"date-parts":[[2023,6,26]]},"assertion":[{"value":"13 April 2022","order":1,"name":"received","label":"Received","group":{"name":"ArticleHistory","label":"Article History"}},{"value":"1 May 2023","order":2,"name":"revised","label":"Revised","group":{"name":"ArticleHistory","label":"Article History"}},{"value":"15 May 2023","order":3,"name":"accepted","label":"Accepted","group":{"name":"ArticleHistory","label":"Article History"}},{"value":"26 June 2023","order":4,"name":"first_online","label":"First Online","group":{"name":"ArticleHistory","label":"Article History"}}]}}