Direct numerical simulation of hypersonic boundary-layer flow on a flared cone

DOI10.1007/s001620050080zbMath0906.76033OpenAlexW2020487291MaRDI QIDQ1268457

C. David Pruett, Chau-Lyan Chang

Publication date: 1998

Published in: Theoretical and Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s001620050080

zbMATH Keywords

frequency spectraadverse streamwise pressure gradienteffects of flared afterbodyGoertler modesMach 6 flownonzero streamwise surface curvatureparabolized stability equationprimary instability

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Parallel shear flows in hydrodynamic stability (76E05) Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (7)

Instability-wave propagation in boundary-layer flows at subsonic through hypersonic Mach numbers ⋮ Interactions between second mode and low-frequency waves in a hypersonic boundary layer ⋮ Direct numerical simulations of hypersonic boundary-layer transition for a flared cone: fundamental breakdown ⋮ Dilatational-wave-induced aerodynamic cooling in transitional hypersonic boundary layers ⋮ Assessment of inflow boundary conditions for compressible turbulent boundary layers ⋮ Newly identified principle for aerodynamic heating in hypersonic flows ⋮ Observation-infused simulations of high-speed boundary-layer transition

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