publication . Article . 1994

Hypersonic aerodynamics on thin bodies with interaction and upstream influence

A. Farid Khorrami; Frank T. Smith;
Open Access
  • Published: 01 Oct 1994 Journal: Journal of Fluid Mechanics, volume 277, pages 85-108 (issn: 0022-1120, eissn: 1469-7645, Copyright policy)
  • Publisher: Cambridge University Press (CUP)
  • Country: United Kingdom
<jats:p>In the fundamental configuration studied here, a steady hypersonic free stream flows over a thin sharp aligned airfoil or flat plate with a leading-edge shock wave, and the flow field in the shock layer (containing a viscous and an inviscid layer) is steady laminar and two-dimensional, for a perfect gas without real and high-temperature gas effects. The viscous and inviscid layers are analysed and computed simultaneously in the region from the leading edge to the trailing edge, including the upstream-influence effect present, to determine the interactive flow throughout the shock layer and the positions of the shock wave and the boundary-layer edge, wher...
Persistent Identifiers
arXiv: Physics::Fluid Dynamics
free text keywords: Mechanical Engineering, Mechanics of Materials, Condensed Matter Physics, Shock wave, Mach number, symbols.namesake, symbols, Inviscid flow, Aerodynamics, Reynolds number, Mechanics, Leading edge, Laminar flow, Materials science, Hypersonic speed
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