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articles
1.Dhanush VITTAL SHENOYorcid_16x16.png, Romain GOJONorcid_16x16.png, Thierry JARDINorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2023).
Angle-of-attack and Mach number effects on the aeroacoustics of an SD7003 airfoil at Reynolds number 60,000
Int. J. Aeroacoustics 22, 131–152. doi:10.1177/1475472X221150173 doi.ico hal.ico openalex-16x16.png
2.Francesco SCARANOorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Romain GOJONorcid_16x16.png, Xavier CARBONNEAUorcid_16x16.png, Erwin Ricky GOWREEorcid_16x16.png (2022).
Modification of a turbulent boundary layer by circular cavities
Phys. Fluids 34, 065134 (15 pages). doi:10.1063/5.0091110 doi.ico hal.ico openalex-16x16.png
3.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2019).
Effects of the angle of impact on the aeroacoustic feedback mechanism in supersonic impinging planar jets
Int. J. Aeroacoustics 18, 258–278. doi:10.1177/1475472X18812808 doi.ico hal.ico openalex-16x16.png
4.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Mihai MIHAESCU (2018).
Oscillation modes in screeching jets
AIAA J. 56, 2918–2924. doi:10.2514/1.J056936 doi.ico hal.ico openalex-16x16.png
5.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2018).
Flow features near plate impinged by ideally expanded and underexpanded round jets
AIAA J. 56, 445–457. doi:10.2514/1.J056421 doi.ico hal.ico openalex-16x16.png
6.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2017).
Numerical study of the flow and the near acoustic fields of an underexpanded round free jet generating two screech tones
Int. J. Aeroacoustics 16, 603–625. doi:10.1177/1475472X17727606 doi.ico hal.ico openalex-16x16.png
7.Christophe BOGEYorcid_16x16.png, Romain GOJONorcid_16x16.png (2017).
Feedback loop and upwind-propagating waves in ideally expanded supersonic impinging round jets
J. Fluid Mech. 823, 562–591. doi:10.1017/jfm.2017.334 doi.ico hal.ico openalex-16x16.png
8.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2017).
Flow structure oscillations and tone production in underexpanded impinging round jets
AIAA J. 55, 1792–1805. doi:10.2514/1.J055618 doi.ico hal.ico openalex-16x16.png
9.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2016).
Investigation of tone generation in ideally expanded supersonic planar impinging jets using large-eddy simulation
J. Fluid Mech. 808, 90–115. doi:10.1017/jfm.2016.628 doi.ico hal.ico openalex-16x16.png
 
thèses/hdr
1.Dhanush VITTAL SHENOYorcid_16x16.png (dir.: Romain GOJON, Thierry JARDIN, Marc C. JACOB) (2023).
Aeroacoustic study of low Reynolds number rotors using Large Eddy Simulations
Thèse Institut Supérieur de l'Aéronautique et de l'Espace
2.Romain GOJONorcid_16x16.png (dir.: Christophe BOGEY) (2015).
Etude de jets supersoniques impactant une paroi par simulation numérique. Analyse aérodynamique et acoustique des mécanismes de rétroaction
Thèse École centrale de Lyon
 
communications avec actes
1.Dhanush VITTAL SHENOYorcid_16x16.png, Romain GOJONorcid_16x16.png, Thierry JARDINorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2022).
Aeroacoustic study of low Reynolds/low Mach number rotor using LES
56th 3AF International Conference on Applied Aerodynamics, Toulouse, France. hal.ico
In: proceeding of the 56th 3AF International Conference on Applied Aerodynamics, Association Aéronautique & Astronautique de France (AAAF), , Paper n°FP44-2022 (8 pages). hal.ico
2.Dhanush VITTAL SHENOYorcid_16x16.png, Romain GOJONorcid_16x16.png, Thierry JARDINorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2021).
Numerical study of flow-acoustic interactions over an SD7003 airfoil at transitional Reynolds numbers
55th 3AF International Conference on Applied Aerodynamics, virtual, France. hal.ico
In: Proceedings of the 55th 3AF International Conference on Applied Aerodynamics, Association Aéronautique & Astronautique de France (AAAF), , Paper n°FP69-2020 (7 pages). hal.ico
*.Yeongmin JO, Thierry JARDINorcid_16x16.png, Romain GOJONorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Jean-Marc MOSCHETTAorcid_16x16.png (2019).
Prediction of noise from low Reynolds number rotors with different number of blades using a non-linear vortex lattice method
25th AIAA/CEAS Aeroacoustics Conference, Delft, Netherlands. doi:10.2514/6.2019-2615 doi.ico hal.ico
In: Proceedings of the 25th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, Paper n°2019-2615 (13 pages). doi:10.2514/6.2019-2615 doi.ico hal.ico
3.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2015).
Large-eddy simulation of supersonic planar jets impinging on a flat plate at an angle of 60 to 90 degrees
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2209 doi.ico hal.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-2209 doi.ico hal.ico
AIAA-2015-2209
4.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2015).
Large-eddy simulation of underexpanded round jets impinging on a flat plate 4 to 9 radii downstream from the nozzle
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2210 doi.ico hal.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-2210 doi.ico hal.ico
AIAA-2015-2210
5.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2015).
Simulation numérique du rayonnement acoustique de jets ronds supersoniques impactant une paroi
CFM 2015 : Congrès Français de Mécanique, Lyon, France.
In: Alain COMBESCURE (Ed.), Michel LANCE (Ed.), Actes du 22ème Congrès Français de Mécanique, Association Française de Mécanique, Courbevoie.
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