Rotorcraft comprehensive code assessment for blade–vortex interaction conditions
Autor: | Jacopo Serafini, Gianluca Romani, Massimo Gennaretti, Giovanni Bernardini |
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Přispěvatelé: | Gennaretti, M., Bernardini, G., Serafini, J., Romani, G. |
Rok vydání: | 2018 |
Předmět: |
020301 aerospace & aeronautics
business.industry Computer science Aerospace Engineering 02 engineering and technology Aerodynamics Wake Solver Aeroelasticity 01 natural sciences 010305 fluids & plasmas 0203 mechanical engineering Fuselage 0103 physical sciences Aeroacoustics Aerospace engineering business Boundary element method Wind tunnel |
Zdroj: | Aerospace Science and Technology. 80:232-246 |
ISSN: | 1270-9638 |
DOI: | 10.1016/j.ast.2018.07.013 |
Popis: | The scope of this paper is the presentation of the computational methodologies applied in the comprehensive code for rotorcraft developed in the last years at Roma Tre University, along with the assessment of its prediction capabilities focused on flight conditions characterized by strong blade–vortex interactions. Boundary element method approaches are applied for both potential aerodynamics and aeroacoustics solutions, whereas a harmonic-balance/modal approach is used to integrate the rotor aeroelastic equations. The validation campaign of the comprehensive code has been carried out against the well-known HART II database, which is the outcome of a joint multi-national effort aimed at performing wind tunnel measurements of loads, blade deflection, wake shape and noise concerning a four-bladed model rotor in low-speed descent flight. Comparisons with numerical simulations available in the literature for the same test cases are also presented. It is shown that, with limited computational cost, the results provided by the Roma Tre aero-acousto-elastic solver are in good agreement with the experimental data, with a level of accuracy that is in line with the state-of-the-art predictions. The influence of the vortex core modeling on aerodynamic predictions and the influence of the inclusion of the fuselage shielding effect on aeroacoustic predictions are discussed. |
Databáze: | OpenAIRE |
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