ICJWSF 2024

Proceedings

Paper IDLastnameNameAffiliationPaper TitleTrackPaper
28InagakiAyumuNational Institute of Technology Oita CollegeMixing Phenomenon Of Multiple Jets Arranged In The Circular Array Of 5 RowsFree and Confined JetsDownload PDF
43OsanoShunTokyo city universityPerformance And Operational Stability Of Axial-Flow Fan With Upstream FilterPassive and Active Flow ControlDownload PDF
48VashishthaAshishSouth East Technological University, Carlow CampusNumerical Investigation Of Non-Premixed Oblique Detonation Operations In Scramjet CombustorCombustion and detonationDownload PDF
20MiauJiun-JihNational Cheng Kung UniversityEvolution Of Flow Around A Finite Circular Cylinder In The Critical Transition RangeWake FlowsDownload PDF
73AndoToshitakeGraduate School of Engineering, Mie UniversityLoss Reduction In The Flow Through An Elbow Tube With Sharp-Edged Corner By Using A Weir-Shaped ObstaclePassive and Active Flow ControlDownload PDF
90BacciTommasoUniversity of FlorenceCharacterization Of The Turbulence Intensity Generated By Passive Grids In Compressible FlowsCompressible FlowsDownload PDF
71MuramatsuAkinoriNihon UniversityFlow Field For Merging Of Four Vortex Rings In A Round Jet Acoustically Excited By A Sinusoidal WaveVortex flowsDownload PDF
74MuramatsuAkinoriNihon UniversityHelical Mode Formed In The Initial Region Of A Round Jet By Synthetic JetsPassive and Active Flow ControlDownload PDF
84HaishiSeiKyushu Institute of TechnologyDynamic Behavior Of Vortex Rings And Characteristics Of Dynamic Forces Formed By Elastic Butterfly WingFluid-structure interactionDownload PDF
78BolognaVirginiaUniversità degli Studi di GenovaAnalysis Of The Shear Layer Instability Process Of A Laminar Separation Bubble By Means Of Dynamic Mode Decomposition TechniqueShear flowsDownload PDF
62BalarasEliasGeorge Washington University Effect Of Different Tessellation Modifications Of Bluff Bodies On Boundary Layer TransitionPassive and Active Flow ControlDownload PDF
79AkagiFujioFukuoka universityNumerical Study Of The Effect Of Ambient Air Oxygen Concentration On The Combustion Behaviour Of Fuel FilmsCombustion and detonation
Download PDF
46MorelloMarioDipartimento di Ingegneria Civile e Industriale (Università di Pisa)Flow Over A 5:1 Rectangular Cylinder At Moderate Reynolds Numbers: Comparison Between Dns, Les, And ExperimentsWake FlowsDownload PDF
76EckMattiasTechnische Universität BerlinReconstruction Of A Continuous Flow Field From Discrete Experimental Data Points Using Physics-Informed Neural NetworksSwirling, shear and wake flowsDownload PDF
38MariottiAlessandro Dipartimento di Ingegneria Civile e Industriale, Università di PisaImpact Of Unsteady Inflow On The Flow Features Of Elongated Rectangular CylindersWake FlowsDownload PDF
29HuangHo-TseNational Cheng Kung UniversityPiv On Cavity Flame Holder In Supersonic FlowCompressible FlowsDownload PDF
80SandriUmbertoUniversity of FlorenceInvestigation Of The Flow Field Morphology Of Film Cooling In Supersonic FlowFree and Confined JetsDownload PDF
60GolliardThomasKTH Royal Institute of Technology, FLOWAnalysis Of The Vorticity Contributions For A Swirling, Supersonic Aerospike Nozzle JetAeroacoustics and NoiseDownload PDF
86IzawaSeiichiroUniversity of ToyamaDynamic Response Of An Inverted Flag Subjected To A Cylinder WakeFluid-structure interactionDownload PDF
45DiepstratenNickEindhoven University of TechnologyModeling Of Non-Premixed Hydrogen Jet Combustion In An Argon/Oxygen Environment Via Direct And Reynold’s Averaged Numerical SimulationsCombustion and detonationDownload PDF
61PinelliLorenzoUniversity of Florence - Department of Industrial Engineering Numerical Analysis Of Combustor Burn-Through Representative JetFree and Confined JetsDownload PDF
87CastelliNiccolo'University of FlorenceNumerical Prediction Of The Heat Loads On A Turbine Vane Test Case: Assessment Of Rans Approaches CapabilitiesHeat TransferDownload PDF
88GaleottiSofiaUniversity of FlorenceHeat Transfer Coefficient And Adiabatic Effectiveness Measurements On A Nozzle Guide Vane With A Double Row Of Cylindrical HolesHeat TransferDownload PDF
44YokohamaMitsuruTokyo university of scienceVisualization And Measurement Of High-Temperature And High-Speed Gas-Solid Two-Phase JetMultiphase FlowsDownload PDF
36HirumaTakayaTokyo city univercityFlow Visualization On Curved Wall Synthetic JetPassive and Active Flow ControlDownload PDF
42SatoRyuichiTokyo City UniversityInfluence Of Spanwise Velocity Distribution On Flow Instability In Inward Swirling FlowPassive and Active Flow ControlDownload PDF
35ToshihiroFujiiTokyo city universityFeasibility Study On Development Of Return Guide Vane Using Jet Flow For Compact Multi-Stage Centrifugal CompressorsPassive and Active Flow ControlDownload PDF
89
RunnooChoomaneePPrime Institute, CNRS, ISAE-ENSMA, Poitiers UniversityCyclic Re-Ignition Phenomena In Constant Volume CombustorsCombustion and detonationDownload PDF
73ÖstmanMartinLuleå University of TechnologyControl Of Hydrogen Jet Mixing Through Use Of Coaxial Air JetFree and Confined JetsDownload PDF
69WeiHongyiTU BerlinExperimental Analysis Of Boundary Condition Effects On The Pressure Field Within An RdcCombustion and detonationDownload PDF
77
WuMutianTokyo University of ScienceNumerical Investigation Of Sliding Motion And Flow Field Changes In Snow Accretion On Wire Using Particle-Based MethodFluid-structure interactionDownload PDF
65EzekwesiliRoselineTechnische Universität (Berlin Germany), Institut P’CNRS (Poitiers France), ISAE-ENSMA (Poiters, France)Experimental Analysis Of End-Gas Temperature Effect On Spontaneous Detonation Development Mechanisms For A Hydrogen/N-Decane MixtureCombustion and detonationDownload PDF
19ChenYu-HsiangNational Cheng Kung UniversityStatistical Analysis Of Flow Field Patterns In Critical Transition Of A Finite Cylinder Using An Adaptive Threshold MethodWake flowsDownload PDF
33MichiokaTakenobuKindai UniversityTurbulent Coherent Structures Around An Array Of BlocksVortex flowsDownload PDF
39ChenYu-HsinDepartment of Aeronautics and Astronautics, College of Engineering, National Cheng Kung University, Tainan, TaiwanReynolds Number Effects On The Vortex State Switch Of An Ucav ModelVortex flowsDownload PDF
54SakashitaTakumiThe University of KitakyushuQuantitative Flow Visualization Of An Elliptic Underexpanded Sonic Jet By RstCompressible flowsDownload PDF
56NishiRyukiUniversity of KitakyushuLarge Eddy Simulation Of Underexpanded Microjets From A Square Supersonic NozzleCompressible FlowsDownload PDF
55MoritaItsukiThe University Of KitakyushuQuantitative Flow Visualization Of A Square Underexpanded Microjet By RstCompressible FlowsDownload PDF
51UenoHiromuThe University of KitakyushuQuantitative Flow Visualization Of Supersonic Jets From An Axisymmetric Laval Nozzle By MziCompressible FlowsDownload PDF
85MarukawaYusukeTokyo University of ScienceEffect Of Electrode Amplitude On Flow Separation Suppression By Multi-Wavy Plasma ActuatorPassive and Active Flow ControlDownload PDF
59GulencGamzeMiddle East Technical University/TUSAS Engine Industries Inc.Numerical Investigation Of Forward/Backward Coolant Injection For Effusion Cooling MethodHeat TransferDownload PDF
34CohenJacobTechnionReduction Of Two-Dimensional Cavity Flow Oscillations At Supersonic Speed By Curving Its Rear FaceCompressible FlowsDownload PDF
73KatoNazuku FUKUDA METAL FOIL & POWDER CO., LTD.Melt Damage To Gas Nozzle Tip In Close-Coupled Gas AtomizationFree and Confined JetsDownload PDF
63PippariHaricharanDepartment of Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur 208016, IndiaHeat Transfer Study Of Obliquely Impinging Jet Cooling A Hot Surface By Using Green Spectrum Based Temperature Sensitive PaintHeat TransferDownload PDF
24KimuraMotoakiDepartment of Mechanical Engineering, College of Science & Technology, Nihon UniversityBehavior Of Chemically Active Species In Premix Burner Using Dbd Plasma ActuatorCombustion and detonationDownload PDF
93KajitaniNaokiKanazawa universityActive Flow Control Of A 2:1 Rectangular Jet Using Dielectric Barrier Discharge Plasma ActuatorsPassive and Active Flow ControlDownload PDF
37SugiyamaKazukiGraduate School of Science and Engineering, Toyo UniversityHemodynamic Effects Of The Unique Network Topology Of Hawaiian Flies’ Wing VeinsPassive and Active Flow ControlDownload PDF
18IsonoTatsushiJapan Aerospace Exploration AgencyOn Effect Of Cell Base Width On Thrust Performance Of A Scramjet External NozzleCombustion and detonationDownload PDF
91OshkaiPeterDepartment of Mechanics Engineering, College of Engineering, University of Victoria, British Colombia, CanadaHigh-Fidelity Analysis Of Propeller-Rudder System Acoustic Signatures In A Full-Scale Marine Vessel: Underwater Radiated Noise Spectra From Wake Structures And CavitationMultiphase FlowsDownload PDF
64ToshihikoShakouchiProfessor, Emeritus, Mie Univerosty, JapanThrust Vector Control Of Supersonic Jet By Movable And Non-Movable Coanda NozzlesPassive and Active Flow ControlDownload PDF
25SemlitschBernhardTU WienNumerical Prediction Of Flow Induced Vibrations In Underflow Sluice GatesMultiphase FlowsDownload PDF
17ChangKeh-ChinProfessor Emeritus, Department of Aeronautics and Astronautics, National Cheng Kung UniversityAnalysis On Evolution Of The Energy Contribution For Coherent Structure In Cylindrical Near-Wake Flow Using Proper Orthogonal DecompositionWake FlowsDownload PDF
52SemlitschBernhardTU WienModelling Leading Edge Erosion Of Wind Turbine BladesFluid machineryDownload PDF
72TagliaferriMauroUniversity of FlorenceHigh-Speed Rdc Data Averaging Through Dynamic TimewarpingCombustion and DetonationDownload PDF
83LalizelGildasISAE-ENSMAExperimental Investigation Of Novel Gas Turbine Film Cooling Configurationusing Phosphor ThermometryHeat TransferDownload PDF
82SridharaShreyas RamanagarUniversity of FlorenceThe Effect Of Compound Angled Holes On A Film Cooled Rotating Detonation CombustorCombustion and DetonationDownload PDF
30Szu-IYehNational Cheng Kung University, TaiwanNumerical Study Of Fish Scales Structure On The Flow Loss Reduction In Compressor CascadeFluid MachineryDownload PDF
49BhideKalyaniUniversity of CincinnatiVorticity And Enstrophy Transport In Rectangular Supersonic JetsFree and confined jetsDownload PDF
50GutmarkEphraimUniversity of CincinnatiFlow And Acoustics By Shock-Turbulence Interaction In Twin-Jets ConfigurationsFree and confined jetsDownload PDF
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