Steady flow in the laminar boundary layer of a gas
From MaRDI portal
Publication:5791495
DOI10.1098/rspa.1949.0153zbMath0034.11503OpenAlexW2075508754MaRDI QIDQ5791495
Publication date: 1949
Published in: Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1098/rspa.1949.0153
Related Items (9)
Three-dimensional, rotational flamelet closure model with two-way coupling ⋮ Development and separation of a compressible laminar boundary layer under the action of a very sharp adverse pressure gradiant ⋮ Diffusion flame in a two-dimensional, accelerating mixing layer ⋮ Mean flow effects on the linear stability of compressible planar jets ⋮ Effects of a sharp pressure rise on a compressible laminar boundary layer, when the Prandtl number is σ = 0.72 ⋮ Prediction of local skin-friction coefficient by transformation of the compressible boundary layer with heat transfer ⋮ Ähnliche Lösungen bei kompressiblen Grenzschichten mit Wärmeübergang und Absaugen oder Ausblasen ⋮ Mixing and combustion in a laminar shear layer with imposed counterflow ⋮ Inward swirling flamelet model
This page was built for publication: Steady flow in the laminar boundary layer of a gas
