Synthesis of the thickness effect in the case of flow past a slender delta wing with leading edge vortices

DOI10.1007/BF01175940zbMath0411.76007MaRDI QIDQ1259489

K. Appert

Publication date: 1979

Published in: Acta Mechanica (Search for Journal in Brave)

zbMATH Keywords

conformal transformationsthickness effectflow past a slender delta wingleading edge vorticesMangler and Smith's mathematical modelsemicircular cone

Mathematics Subject Classification ID

Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Two-dimensional potential theory (31A99)

Cites Work

• A theory of the flow past a slender delta wing with leading edge separation
• The inner viscous solution for the core of a leading-edge vortex
• The flow field near the centre of a rolled-up vortex sheet

This page was built for publication: Synthesis of the thickness effect in the case of flow past a slender delta wing with leading edge vortices