Incipient separation in laminar, ramp-induced shock-wave/boundary-layer interactions is examined using numerical solutions of the triple-deck equations and the full set of governing equations for compressible flows. Validation of the numerical methods is presented and the results are compared. A new comparison between solutions to the triple-deck equations and the compressible Navier–Stokes equations is presented. It was found that the triple-deck trends qualitatively match the trends produced by numerical solutions to the compressible Navier–Stokes equations. An expression for true incipient separation is derived and the trends are discussed.
Incipient Separation in Laminar Ramp-Induced Shock-Wave/Boundary-Layer Interactions
AIAA Journal ; 56 , 2 ; 524-531
2017-10-19
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Micro-Ramp Control for Oblique Shock Wave / Boundary Layer Interactions
British Library Conference Proceedings | 2007
|