Review



bli ducted fan test  (ONERA The French Aerospace Lab)

 
  • Logo
  • About
  • News
  • Press Release
  • Team
  • Advisors
  • Partners
  • Contact
  • Bioz Stars
  • Bioz vStars
    • 90
      Buy from Supplier

    Structured Review

    ONERA The French Aerospace Lab bli ducted fan test
    Schematic of novel aircraft featuring boundary layer ingesting <t>(BLI)</t> <t>ducted</t> fan propulsion systems.
    Bli Ducted Fan Test, supplied by ONERA The French Aerospace Lab, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
    https://www.bioz.com/product/bli+ducted+fan+test/bli+ducted+fan+test/pmc12081303-68-1-24
    Average 90 stars, based on 1 article reviews
    bli ducted fan test - by Bioz Stars, 2026-09
    90/100 stars

    Images

    1) Product Images from "Aeroacoustics and psychoacoustics characterization of a boundary layer ingesting ducted fan"

    Article Title: Aeroacoustics and psychoacoustics characterization of a boundary layer ingesting ducted fan

    Journal: Npj Acoustics

    doi: 10.1038/s44384-025-00010-z

    Schematic of novel aircraft featuring boundary layer ingesting (BLI) ducted fan propulsion systems.
    Figure Legend Snippet: Schematic of novel aircraft featuring boundary layer ingesting (BLI) ducted fan propulsion systems.

    Techniques Used:

    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. ).
    Figure Legend 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. ).

    Techniques Used:

    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.
    Figure Legend 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.

    Techniques Used:

    Related Articles

    other:

    Article Title: Aeroacoustics and psychoacoustics characterization of a boundary layer ingesting ducted fan
    Article Snippet: The BLI ducted fan test is designed and developed to demonstrate the partially-buried engines in the aerospace sector, e.g., the propulsion unit in the ONERA NOVA configuration (see Fig. ).



    Similar Products

    bli ducted fan test  (ONERA The French Aerospace Lab)
    90
    ONERA The French Aerospace Lab bli ducted fan test
    Schematic of novel aircraft featuring boundary layer ingesting <t>(BLI)</t> <t>ducted</t> fan propulsion systems.
    Bli Ducted Fan Test, supplied by ONERA The French Aerospace Lab, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
    https://www.bioz.com/product/bli+ducted+fan+test/bli+ducted+fan+test/pmc12081303-68-1-24
    Average 90 stars, based on 1 article reviews
    bli ducted fan test - by Bioz Stars, 2026-09
    90/100 stars
    		  Buy from Supplier

    Image Search Results


    Schematic of novel aircraft featuring boundary layer ingesting (BLI) ducted fan propulsion systems.

    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 BLI ducted fan test is designed and developed to demonstrate the partially-buried engines in the aerospace sector, e.g., the propulsion unit in the ONERA NOVA configuration (see Fig. ).

    Techniques:

    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. ).

    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 BLI ducted fan test is designed and developed to demonstrate the partially-buried engines in the aerospace sector, e.g., the propulsion unit in the ONERA NOVA configuration (see Fig. ).

    Techniques:

    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.

    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 BLI ducted fan test is designed and developed to demonstrate the partially-buried engines in the aerospace sector, e.g., the propulsion unit in the ONERA NOVA configuration (see Fig. ).

    Techniques: