Plane and axisymmetric bodies in a flow with the greatest ``critical Mach number

DOI10.1134/S0015462822040073zbMath1497.76074MaRDI QIDQ2172686

V. A. Shapovalov, A. N. Kraĭko

Publication date: 16 September 2022

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

zbMATH Keywords

genetic algorithmdirect optimization methodBézier curveinviscid non-heat-conducting gasimplicit Godunov schemesupersonic zone

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Flow control and optimization for compressible fluids and gas dynamics (76N25) Basic methods in fluid mechanics (76M99)

Related Items (1)

Lift airfoils close to the airfoils in a flow with the maximum ``critical Mach numbers

Cites Work

• Unnamed Item
• Unnamed Item
• Contouring two-sided asymmetric plane maximum-thrust nozzles
• Planar and axially symmetric configurations which are circumvented with the maximum critical Mach number
• On the construction and calculation of optimal nonlifting critical airfoils
• Calculation of the cavitating flow around a circular cone by a subsonic stream of a compressible fluid
• Comparison of the efficiencies of spike and combined annular nozzles
• Nose part of the body of revolution having minimum aerodynamic drag in the range of large subsonic velocities
• Maximum critical Mach number flows around semi-infinite solids of revolution
• Calculation of Subsonic Cavities with Sonic Free Streamlines

This page was built for publication: Plane and axisymmetric bodies in a flow with the greatest ``critical Mach number