Geodesic

Volume 34 (2022) no. 7

Sommaire

Тематический выпуск "Вычислительный эксперимент в аэроакустике"
p. 3-4
Computational and experimental studies of a low-noise aircraft with a laminar wing and engines above the trailing edge of the wing
p. 5-23
Approaches to the numerical simulation of the acoustic field generated by multi-element aircraft wing in high-lift configuration
p. 24-48
Numerical simulation of the evolution of an intense aerodynamic jet in the far-field propagation
p. 49-62
Numerical simulation of turbulent spots evolution in supersonic boundary layer over a plate
p. 63-72
Development of unstructed code for rotating zones based on the CABARET method with improved spectral properties
p. 73-92
Mathematical modelling as an integral part of the wind tunnels experimental methodology
p. 93-112