Geodesic

Volume 19 (2007) no. 8

Sommaire

The reaction of degenerate Bose gas on temperature disturbances in simplified transportation model
p. 3-14
Numerical experiments on acoustic liners
p. 15-21
Numerical calculation of sound absorbing structures (SAS) for modern aircraft engines
p. 22-30
Modeling the time-dependent interaction between a~sonic jet and a~barrier
p. 31-36
Mathematical model and method calculation of aeroacoustic parameters in nonisothermal jets
p. 37-48
Use of transparent boundary conditions for solution of two-dimensional elastodynamics problems with azimuthal anisotropy
p. 49-54
Comparison of nonreflecting boundary conditions as
p. 55-65
Modelling of sound propagation through non-uniform flows of turbulent jets
p. 66-74
Generation of discrete non-reflecting boundary conditions
p. 75-82
Development of approach for air engine tonal noise estimation
p. 83-89
A forestry influence on an acoustical perturbance propagation
p. 90-96
Modeling fan stage acoustic characteristics
p. 97-104
About using transparent boundary conditions in aeroacoustics
p. 105-112
Calculation of sound fields in turbofan engine intakes based on azimuthal fourier decomposition
p. 113-122
Brief review of programm package WHISPAR for solving aeroacoustics problems on structured grids
p. 123-128