Pages that link to "Item:Q416525"
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The following pages link to Noise prediction for a turbulent jet using different hybrid methods (Q416525):
Displaying 15 items.
- Numerical analysis of the acoustic field of reacting flows via acoustic perturbation equations (Q416621) (← links)
- A hybrid prediction method for low-subsonic turbulent flow noise (Q435664) (← links)
- Hybrid prediction of the aerodynamic noise radiated by a rectangular cylinder at incidence (Q1645569) (← links)
- A fully coupled hybrid computational aeroacoustics method on hierarchical Cartesian meshes (Q1648151) (← links)
- Fluid mechanics research at the Institute of Aerodynamics, RWTH Aachen University: from 1912 through 2012 (Q1670026) (← links)
- Dynamic load balancing for direct-coupled multiphysics simulations (Q2294032) (← links)
- Jet noise analysis using an efficient LES/high-order acoustic coupling method (Q2294033) (← links)
- Numerical error analysis with application to transonic propeller aeroacoustics (Q2361963) (← links)
- Noise sources in heated coaxial jets (Q2446533) (← links)
- Prediction of noise generated by a round nozzle jet flow using computational aeroacoustics (Q2845402) (← links)
- On least-order flow representations for aerodynamics and aeroacoustics (Q3168069) (← links)
- Toward accurate hybrid prediction techniques for cavity flow noise applications (Q3654191) (← links)
- Nozzles, turbulence, and jet noise prediction (Q4647331) (← links)
- Reduced-order representation of turbulent jet flow and its noise source (Q5427484) (← links)
- High-fidelity simulations of the aeroacoustic environment of the VEGA launch vehicle at lift-off (Q6093444) (← links)
