Existence of piecewise smooth attached-shock self-similar solutions is established for supersonic Chaplygin gas flow past a conical wing with Λ-shaped cross sections.
Lieberman,Oblique derivative problems in Lipschitz domains
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Supersonic flow of a Chaplygin gas past a conical wing with $\Lambda$-shaped cross sections
Existence of piecewise smooth attached-shock self-similar solutions is established for supersonic Chaplygin gas flow past a conical wing with Λ-shaped cross sections.