Proceedings of the 10th IUTAM Symposium on Laminar-Turbulent Transition

IUTAM Laminar-Turbulent Transition; September 2-6, 2024, Nagano, Japan
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Inhaltsangabe

Turbulent spot measurements: wall-pressure and streamwise-velocity correlation.- DNS Study of Flow Mechanism Contributing to Drag Reduction over Distributed Micro Roughness.- Transition Control for Separated Flow over Airfoil by Periodic Body Forcing.- Axial flow influence on boundary-layer transition on rotating slender cones.- Numerical investigations of the nonlinear stages of hypersonic boundary-layer transition for an ogive geometry.- Instability, transition and turbulence on rotating disks and cones - Quo vadis?.- Investigation of Turbulent Wedge Intermittency with Time-Resolved Temperature-Sensitive Paint.- Boundary-layer instability characteristics of supersonic and hypersonic flows over rotating cones.- Interaction of Crossflow Modes with Forward-Facing Steps: Insights Gained from DNS.- Numerical investigations of stability and transition for a blunt swept flat plate at Mach 10.- Numerical and Experimental Investigations of Transition in a Laminar Separation Bubble.- Experimental study on the mechanism of lateral growth of developed turbulent wedge.- Experimental Study of the Instability Amplitude Effect on Critical Step Heights in Crossflow-Dominated Transition.- Flow state transition process and oblique pattern of Taylor–Couette–Poiseuille flow at a medium cylinder ratio.- New perspectives on instability of laminar separation bubbles: have we been missing something important?.- Stability analysis of recirculation bubble flow in a viscoelastic fluid.- Linear and nonlinear response of high-speed boundary layers to continuous stochastic forcing.- Experimental investigation of bluntness effects on transition on a 7-degree blunted cone.- Simulation of K-type and H-type Transition Using the Nonlinear One-Way Navier-Stokes Approach.- Generative machine-learning methods to predict the wake of a distributed roughness patch in a hypersonic boundary-layer flow.- Airfoil trailing-edge tonal noise reduction by roughness elements.- Numerical and experimental study on the freestream-turbulence dependency of turbulent transition processes on a swept flat plate.- Computations of Turbulent Transition in Hypersonic Boundary Layer with Reduced Artificial Dissipation.- Experimental investigation on boundary-layer streaks induced by grid-generated free-stream turbulence.- Global stability analysis of installed jets.- Infrared thermographic evaluation of wall-temperature streak in the free-stream turbulence transition scenario.- Adjoint-Based Approach for Prediction of Non-Modal Growth in Spatially Evolving Flows.- Interscale energy transfer in a transitional swept-wing boundary layer...

Produktdetails
  • Erscheinungsdatum: 22.01.2026
  • Autor/Autorin: Kentaro Kato
  • Reihe: Engineering (R0)
  • Format: E-Book
  • Dateiformat: PDF
  • Kopierschutz: Wasserzeichen
  • Dateigröße: 34.3 MB
  • Verlag: SPRINGER
  • Sprache: Englisch
  • Umfang: 340 Seiten
  • ISBN: 9789819698295
  • Lieferung: Sofort per Download
  • Hinweis: Sofort per Download lieferbar. Kein physischer Versand.
  • Kompatibilität: Lesbar auf Geräten und Apps mit PDF-Unterstützung.
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