On unsteady boundary-layer separation in supersonic flow. Part 1. Upstream moving separation point
From MaRDI portal
Publication:2891676
DOI10.1017/jfm.2011.104zbMath1241.76339OpenAlexW2316732000MaRDI QIDQ2891676
Dai Araki, R. Yapalparvi, Anatoly I. Ruban, Jitesh S. B. Gajjar
Publication date: 15 June 2012
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/jfm.2011.104
Related Items
Incompressible boundary layer with counterflows at a given pressure gradient ⋮ Double-deck structure of the boundary layer in the problem of a compressible flow along a plate with small irregularities on the surface ⋮ Double-deck structure in the problem of a compressible flow along a plate with small localized irregularities on the surface ⋮ Singularity formation in an incompressible boundary layer on an upstream moving wall under given external pressure ⋮ On quasi-steady boundary-layer separation in supersonic flow. Part 2. Downstream moving separation point ⋮ Exact theory of material spike formation in flow separation ⋮ Towards the detection of moving separation in unsteady flows ⋮ Material spike formation in highly unsteady separated flows ⋮ Free interaction of the flow in a laminar boundary layer with an upstream moving expansion wave ⋮ Numerical solution of unsteady boundary-layer separation in supersonic flow: upstream moving wall
Cites Work
- The spontaneous generation of the singularity in a separating laminar boundary layer
- The laminar boundary layer on a circular cylinder started impulsively from rest
- Computer extension and analytic continuation of Blasius’ expansion for impulsive flow past a circular cylinder
- Unsteady viscous flow in the vicinity of a stagnation point
- Unsteady boundary layers with an intelligent numerical scheme
- Vortex-induced boundary-layer separation. Part 1. The unsteady limit problem Re [rightward arrow [infty infinity]]
- Unsteady laminar separation over impulsively moved cylinders
- Asymptotic Theory of Separated Flows
- Unsteady separation from the leading edge of a thin airfoil
- Shock wave interaction with a viscous wake in supersonic flow
- Once again on the supersonic flow separation near a corner
- Unsteady separation and heat transfer upstream of obstacles
- Self-induced separation
- On the flow near the trailing edge of a flat plate II
- Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
- Boundary-layer development at a two-dimensional rear stagnation point
- Boundary-Layer Separation From Downstream Moving Boundaries
- THE INITIAL FLOW PAST AN IMPULSIVELY STARTED CIRCULAR CYLINDER
- Flow past an impulsively started circular cylinder
- Boundary-layer growth near a rear stagnation point
- ON LAMINAR BOUNDARY-LAYER FLOW NEAR A POSITION OF SEPARATION
- Wachstum der laminaren Grenzschicht an schräg angeströmten Zylindern bei Anfahrt aus der Ruhe
