Calculation of supersonic flow around V-shaped wings by the fitting method

DOI10.1007/BF01014010zbMath0269.76042OpenAlexW2036513135MaRDI QIDQ758383

V. I. Lapygin

Publication date: 1973

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

Full work available at URL: https://doi.org/10.1007/bf01014010

Mathematics Subject Classification ID

Supersonic flows (76J20)

Related Items

Wave drag of slender star-shaped bodies at moderate supersonic flight velocities ⋮ Submerged shocks in conical gas flows in the presence of a Mach shock-wave configuration ⋮ The mode of attached compression shock at edges of a V-shaped wing ⋮ Structure of supersonic inviscid nonsymmetric conical flow around a V-wing

Cites Work

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• An evaluation of several differencing methods for inviscid fluid flow problems
• A time-dependent computational method for blunt body flows.
• A Method for the Numerical Calculation of Hydrodynamic Shocks