Global PNS solutions for subsonic strong interaction flow over a cone- cylinder-boattail configuration
DOI10.1016/0045-7930(83)90018-XzbMath0526.76049OpenAlexW2062438047MaRDI QIDQ594703
Publication date: 1983
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/0045-7930(83)90018-x
large Reynolds numbersstrong pressure interactionflow past cone-cylinder-boattail configurationglobal boundary-layer relaxation procedurelarge recirculation regionsmarching proceduresemi-elliptic or parabolizedstrong viscous-inviscid interaction
Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Basic methods in fluid mechanics (76M99)
Related Items (5)
Cites Work
- Global PNS solutions for subsonic strong interaction flow over a cone- cylinder-boattail configuration
- Non-Navier Stokes viscous flow computations
- Viscous flow over a cone at moderate incidence. I: Hypersonic tip region
- Numerical Simulation of Steady Supersonic Viscous Flow
- Three-Dimensional Supersonic Viscous Flow over a Cone at Incidence
- Calculation of the Flow on a Cone at High Angle of Attack
- Second-order boundary-layer effects in hypersonic flow past axisymmetric blunt bodies
- Hypersonic viscous flow over slender bodies with sharp leading edges.
- On boundary layers and upstream influence. I. A comparison between subsonic and supersonic flows
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