Pages that link to "Item:Q2778689"

The following pages link to Aeroacoustic integral methods, formulation and efficient numerical implementation. (Q2778689):

Displaying 19 items.

• Surface integral analogy approaches for predicting noise from 3D high-lift now-noise wings (Q318406) (← links)
• Source-time dominant aeroacoustics (Q597092) (← links)
• An accurate and efficient computational method for time-domain aeroacoustic scattering (Q776706) (← links)
• A nonintrusive reduced basis method applied to aeroacoustic simulations (Q904229) (← links)
• Vortex particle methods in aeroacoustic calculations (Q950370) (← links)
• Aeroacoustic modeling of complex flow problems. I: Domain decomposition method for the reduced wave equation (Q1348618) (← 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)
• Numerical simulations of helicopter aerodynamics and acoustics (Q1919397) (← links)
• A CFD/CAA coupling method applied to jet noise prediction (Q2016144) (← links)
• Numerical error analysis with application to transonic propeller aeroacoustics (Q2361963) (← links)
• Extension of Kirchhoff's formula to radiation from moving surfaces (Q2879842) (← links)
• Improved integral formulae for supersonic reconstruction of the acoustic field (Q3122005) (← links)
• Optimized compact filtering schemes for computational aeroacoustics (Q3636915) (← links)
• Aeroacoustic Boundary Element Method Using Analytical/Numerical Matching (Q4363374) (← links)
• (Q4781663) (← links)
• Investigation of integral surface formulations for acoustic post-processing of unsteady aerodynamic jet simulations (Q5706518) (← links)
• A 2D frequency domain finite element formulation for solving the wave equation in the presence of rotating obstacles (Q6072637) (← links)
• Hybrid Aeroacoustic Computations: State of Art and New Achievements (Q6201452) (← links)