Nose part of the body of revolution having minimum aerodynamic drag in the range of large subsonic velocities

DOI10.1134/S0015462822010074zbMath1501.76070OpenAlexW4220800840MaRDI QIDQ2086787

A. P. Mazurov, S. A. Takovitskij

Publication date: 26 October 2022

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

Full work available at URL: https://doi.org/10.1134/s0015462822010074

zbMATH Keywords

Navier-Stokes equationstransonic flowlocal linearizationaxisymmetric noseminimal aerodynamic dragRyabouchinsky half-cavitytruncated power-law body

Mathematics Subject Classification ID

Transonic flows (76H05) General aerodynamics and subsonic flows (76G25) Flow control and optimization for compressible fluids and gas dynamics (76N25) Compressible Navier-Stokes equations (76N06)

Related Items (1)

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

Cites Work

• Unnamed Item
• Analytical solution in the problem of constructing axisymmetric noses with minimum wave drag
• Planar and axially symmetric configurations which are circumvented with the maximum critical Mach number
• Optimal axisymmetric noses of bodies in a flow. Calculations and experiments
• Analytical solution to the wave-drag minimization problem for an axisymmetric fore-body using local linearization
• Newton's problem of the optimal forebody: history of the solution
• Axisymmetric nose shapes of specified aspect ratio, optimum or close to optimum with respect to wave drag

This page was built for publication: Nose part of the body of revolution having minimum aerodynamic drag in the range of large subsonic velocities