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Image Search Results
Journal: Npj Acoustics
Article Title: Aeroacoustics and psychoacoustics characterization of a boundary layer ingesting ducted fan
doi: 10.1038/s44384-025-00010-z
Figure Lengend Snippet: Schematic of novel aircraft featuring boundary layer ingesting (BLI) ducted fan propulsion systems.
Article Snippet: The
Techniques:
Journal: Npj Acoustics
Article Title: Aeroacoustics and psychoacoustics characterization of a boundary layer ingesting ducted fan
doi: 10.1038/s44384-025-00010-z
Figure Lengend Snippet: a Zero pressure gradient and ( b ) adverse pressure gradient flow . The boundary layer develops over a curved airframe that resembles the rear fuselage of the ONERA NOVA and NASA Aurora D8 aircraft concepts featuring boundary layer ingesting (BLI) ducted fans (see Fig. ).
Article Snippet: The
Techniques:
Journal: Npj Acoustics
Article Title: Aeroacoustics and psychoacoustics characterization of a boundary layer ingesting ducted fan
doi: 10.1038/s44384-025-00010-z
Figure Lengend Snippet: a Boundary layer ingesting (BLI) ducted fan test rig inside the anechoic chamber of the aeroacoustics wind tunnel facility at the University of Bristol. b Schematic representation of the experimental setup, illustrating the positioning of the curved S-plate, ducted fan, and microphone array; and ( c) Measurement layout on the curved S-plate, showing the distribution of pressure taps along the streamwise direction and a dense grid of hot-wire measurement points (~150 points per streamwise location) for detailed velocity field analysis.
Article Snippet: The
Techniques: