Optimal axisymmetric noses of bodies in a flow. Calculations and experiments

DOI10.1134/S0015462818020052zbMath1395.76080MaRDI QIDQ1672392

K. S. P'yankov, N. I. Tillyaeva, I. P. Bol'shiyanov, N. N. Zakharov

Publication date: 10 September 2018

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

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Related Items (2)

Nose part of the body of revolution having minimum aerodynamic drag in the range of large subsonic velocities ⋮ Boundary layer dynamics in a compressible gas. Numerical simulation

Cites Work

• A universal one-equation model for turbulent viscosity
• Axisymmetric nose shapes of specified aspect ratio, optimum or close to optimum with respect to wave drag

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