Asymptotic theory of the flow near the rear end of a slender axisymmetric body
From MaRDI portal
Publication:1339595
DOI10.1007/BF01050047zbMath0810.76017OpenAlexW2035085482MaRDI QIDQ1339595
Publication date: 6 December 1994
Published in: Fluid Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/bf01050047
Related Items (1)
Cites Work
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Triple-deck solutions for subsonic flow past humps, steps, concave or convex corners and wedged trailing edges
- Investigation of selfsimilar solutions describing flows in mixing layers
- Free convection boundary layers near corners and sharp trailing edges
- Non-uniqueness in wakes and boundary layers
- Viscous-inviscid interactions on axisymmetric bodies of revolution in supersonic flow
- Axisymmetric flow past a slender body of finite length
- The Incompressible Laminar Axisymmetric Far Wake
- On the flow near the trailing edge of a flat plate II
- Trailing edge flows
- Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
- ON LAMINAR BOUNDARY LAYERS NEAR CORNERS
This page was built for publication: Asymptotic theory of the flow near the rear end of a slender axisymmetric body