2020
DOI: 10.1007/978-3-030-50436-6_16
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Prediction of the Free Jet Noise Using Quasi-gas Dynamic Equations and Acoustic Analogy

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Cited by 5 publications
(4 citation statements)
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“…In an earlier study [ 28 ], the FWH analogy was also validated using another software using the rod–airfoil interaction. The library has been used to simulate compressible free jets, and the results have been compared favorably to the experimental data using the FWH method [ 29 , 30 ]. It has also been used to simulate the marine propeller noise [ 31 ] and the rotor noise from unmanned arial vehicles [ 32 , 33 ].…”
Section: Methodsmentioning
confidence: 99%
“…In an earlier study [ 28 ], the FWH analogy was also validated using another software using the rod–airfoil interaction. The library has been used to simulate compressible free jets, and the results have been compared favorably to the experimental data using the FWH method [ 29 , 30 ]. It has also been used to simulate the marine propeller noise [ 31 ] and the rotor noise from unmanned arial vehicles [ 32 , 33 ].…”
Section: Methodsmentioning
confidence: 99%
“…The Eulerian part of the model for both of the system equations was verified by solving the various problems such as: (a) shock tube and other discontinuity evolution problems [27,28], (b) the flow around the forward and backward step with super-and subsonic velocities [28,39], (c) flow around blunt bodies at trans-and supersonic velocities [27,28,39], and d) hydrodynamic instabilities development and acoustic noise generation by a transonic jet [40,41]. The libAcoustics library of far-field noise analysis was successfully tested for a number of models (monopole, dipole) and experimental problems [37,40,41]. The verification of the droplet-dynamics model is presented in the next two sections.…”
Section: Verification and Validationmentioning
confidence: 99%
“…The computational mesh was refined in the region from the gas nozzle exit 30D downstream. According to the recommendations presented in [40,41], two meshes for each solver were constructed. It was shown in previous studies that two numerical algorithms required different mesh resolutions to simulate the instabilities arising from the mixing layer of a high-speed jet.…”
Section: Asmentioning
confidence: 99%
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