Pages that link to "Item:Q5706518"
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The following pages link to Investigation of integral surface formulations for acoustic post-processing of unsteady aerodynamic jet simulations (Q5706518):
Displaying 10 items.
- Surface integral analogy approaches for predicting noise from 3D high-lift now-noise wings (Q318406) (← links)
- Computation of a high Reynolds number jet and its radiated noise using large eddy simulation based on explicit filtering (Q1043103) (← links)
- A high-order interpolation for the finite volume method: the coupled least squares reconstruction (Q1625617) (← links)
- Additional terms for the use of Ffowcs Williams and Hawkings surface integrals in turbulent flows (Q1645959) (← links)
- Comparison of surface and volume integral methods for transonic propeller acoustic predictions (Q1739682) (← links)
- A CFD/CAA coupling method applied to jet noise prediction (Q2016144) (← links)
- Development and validation of a phase shift and attenuation free filtering for exploitation of CFD data (Q2361880) (← links)
- Aeroacoustic integral methods, formulation and efficient numerical implementation. (Q2778689) (← links)
- A generalized sound extrapolation method for turbulent flows (Q4559541) (← links)
- A volume integral implementation of the Goldstein generalised acoustic analogy for unsteady flow simulations (Q4585869) (← links)
