Stationary flow past the lower surface of a piecewise planar delta wing with supersonic leading edges

DOI10.1007/BF01409810zbMath0446.76015OpenAlexW2061021298MaRDI QIDQ1146068

S. M. Ter-Minasyants

Publication date: 1979

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01409810

zbMATH Keywords

Hilbert boundary value problemlogarithmic singularitypressure distributionthin winglinearized solutioninflexion linesLighthill's approach

Mathematics Subject Classification ID

Analyticity in context of PDEs (35A20) Boundary values of solutions to elliptic equations and elliptic systems (35J67) Supersonic flows (76J20) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Boundary value problems for linear first-order PDEs (35F15)

Cites Work

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• Supersonic and hypersonic flow with attached shock waves over delta wings
• The diffraction of blast. I
• On Aerodynamics of Blasts
• THE DIFFRACTION AND REFLECTION OF SHOCK WAVES

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