Hypersonic flow of gas over a slender wing of variable shape

DOI10.1007/BF01051255zbMath0456.76050MaRDI QIDQ1150501

S. H. Smith

Publication date: 1979

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

zbMATH Keywords

slender wingEuler-Ampere transformationhalf-inverse problemthin shock layer approach

Mathematics Subject Classification ID

Integro-partial differential equations (45K05) Initial value problems for nonlinear higher-order PDEs (35G25) Supersonic flows (76J20) Hypersonic flows (76K05) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (2)

On mathematical modeling of a hypersonic flow past a thin wing with variable shape ⋮ Numerical modeling of supersonic flow over wings with varying aspect ratio on a broad range of angles of attack using the law of plane sections

Cites Work

• Nonlinear conical flow of a gas
• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY
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