Improving the aerodynamic performance of small-aspect-ratio wings at hypersonic speeds

DOI10.1016/0021-8928(92)90022-ZzbMath0786.76045OpenAlexW2003654337MaRDI QIDQ1314168

V. N. Golubkin, V. V. Negoda

Publication date: 3 March 1994

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(92)90022-z

zbMATH Keywords

angle of attackleading edgelower surfacenext approximation to the Newtonian theory

Mathematics Subject Classification ID

Variational methods applied to problems in fluid mechanics (76M30) Hypersonic flows (76K05)

Related Items (2)

Optimum lifting body shapes in hypersonic flow at high angles of attack ⋮ Lifting wings of optimum shape in a viscous hypersonic stream

Cites Work

• A wing with the maximum lift/drag ratio at supersonic velocity
• A class of three-dimensional, optimum hypersonic wings.
• Unnamed Item

This page was built for publication: Improving the aerodynamic performance of small-aspect-ratio wings at hypersonic speeds