Effect of Reynolds number on a normal shock wave-transitional boundary-layer interaction over a curved surface
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DOI: 10.1007/s00348-019-2824-0
Abstract: The interaction between a normal shock wave and a boundary layer is investigated over a curved surface for a Reynolds number range, based on boundary-layer growing length x, of $$0.44\times 10^6\le \text {Re}_x\le 1.09\times 10^6$$0.44×106≤Rex≤1.09×106.… read more here.
Keywords: layer; normal shock; shock wave; boundary layer ... See more keywords
Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback
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DOI: 10.1155/2020/5313941
Abstract: In order to consider the inlet and engine integrated model of supersonic airliner, the dynamic identification and control of inlet normal shock are studied. The research is based on the bleed air flow rate under… read more here.
Keywords: inlet; normal shock; model; inlet engine ... See more keywords
Normal-Shock/Boundary-Layer Interactions in Transonic Intakes at High Incidence
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DOI: 10.2514/1.j058054
Abstract: During high-incidence maneuvers, shock-wave/boundary-layer interactions can develop over transonic inlet lower lips, significantly impacting aerodynamic performance. Here, a novel experimental rig ... read more here.
Keywords: boundary layer; normal shock; high incidence; layer interactions ... See more keywords