Pages that link to "Item:Q2016144"
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The following pages link to A CFD/CAA coupling method applied to jet noise prediction (Q2016144):
Displaying 12 items.
- Time domain computation of flow induced sound (Q416509) (← links)
- Additional terms for the use of Ffowcs Williams and Hawkings surface integrals in turbulent flows (Q1645959) (← links)
- Concurrent finite element simulation of quadrupolar and dipolar flow noise in low Mach number aeroacoustics (Q1646966) (← links)
- A domain decomposition technique for small amplitude wave interactions with shock waves (Q2124342) (← links)
- Jet noise analysis using an efficient LES/high-order acoustic coupling method (Q2294033) (← links)
- Hybrid methods for airframe noise numerical prediction (Q2576558) (← links)
- Prediction of noise generated by a round nozzle jet flow using computational aeroacoustics (Q2845402) (← links)
- A Coupling Scheme for Direct Numerical Simulations with an Acoustic Solver (Q5427482) (← links)
- Contributions of Computational Aeroacoustics to Jet Noise Research and Prediction (Q5460643) (← links)
- High-fidelity simulations of the aeroacoustic environment of the VEGA launch vehicle at lift-off (Q6093444) (← links)
- Применение акустико-вихревого метода для моделирования шума пропеллера мультикоптера;Application of acoustic-vortex method for CFD-CAA modelling of multicopter noise (Q6165654) (← links)
- A domain decomposition technique for acoustic wave interactions and scattering (Q6189296) (← links)
