Hypersonic flow past a wing at large angles of attack with detached shock wave

DOI10.1007/BF01050004zbMath0598.76073MaRDI QIDQ1080317

V. V. Negoda, V. N. Golubkin

Publication date: 1985

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

zbMATH Keywords

hypersonic flowthermal radiationdelta wingnonequilibrium physicochemical processeslarge angles of attackthin shock layer methodthree-dimensional hypersonic flowwindward surface

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05) Basic methods in fluid mechanics (76M99)

Related Items (1)

Optimization of the shape of a wing in a hypersonic nonequilibrium gas flow

Cites Work

• Hypersonic flow past a delta wing at large angles of attack
• Recent Hypersonic Studies of Wings and Bodies
• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY

This page was built for publication: Hypersonic flow past a wing at large angles of attack with detached shock wave