Numerical simulations of turbulent spots in supersonic boundary layers: Effects of Mach number and wall temperature

Author:

Redford J.A.,Sandham N.D.,Roberts G.T.

Funder

EU through the FP-7 ATLLAS project

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference33 articles.

1. Transition experiments on blunt bodies with isolated roughness elements in hypersonic flight;Reda;Journal of Spacecraft and Rockets,2010

2. Steelant J. LAPCAT: high-speed propulsion technology advances on propulsion technology for high-speed aircraft. Educational Notes RTO-EN-AVT-150. Paper 12: 12-1–12-38 Neuilly-sur-Seine, France: RTO. Available from: 〈http://www.rto.nato.int〉.

3. Shock-wave/boundary-layer interactions in a model scramjet intake;Krishnan;AIAA Journal,2009

4. The laminar-turbulent transition in a boundary layer—Part I;Emmons;Journal of the Aeronautical Sciences,1951

5. Simulations of bypass transition;Jacobs;Journal of Fluid Mechanics,2001

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