Boundary layer in neighborhood of centerline of symmetry with adverse pressure gradients and heat transfer is studied with view toward assessing importance of three-dimensional effects on such boundary layers in hypersonic inlets of airbreathing engines; two approaches are employed; in one, analysis is performed so that parameters describing external flow and surface geometry are restricted to those yielding similar boundary layers; numerical results are presented; second approach is integral method which can be applied for similar and nonsimilar flows. (See also AIAA-ASME -- Hypersonic Ramjet Conference -- Paper 63-115 1963 36 p)
Laminar boundary layer near plane of symmetry of hypersonic inlet
AIAA J
AIAA Journal ; 1 , n 12
1963
9 pages
Article (Journal)
English
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