On the theory of a wing with small aspect ratio in a hypersonic flow

DOI10.1007/BF01089616zbMath0461.76047MaRDI QIDQ1152773

V. N. Golubkin

Publication date: 1980

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

zbMATH Keywords

three-dimensionalsmall aspect ratioflat delta-shaped

Mathematics Subject Classification ID

Gas dynamics (general theory) (76N15) Hypersonic flows (76K05) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (2)

Lifting wings of optimum shape in a viscous hypersonic stream ⋮ Three-dimensional hypersonic gas flow over wings

Cites Work

• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY
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