aerospace testing Search Results


90
ONERA The French Aerospace Lab test facility blade
Test Facility Blade, 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
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ONERA The French Aerospace Lab electron beam irradiation test
Electron Beam Irradiation 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
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Average 90 stars, based on 1 article reviews
electron beam irradiation test - by Bioz Stars, 2026-08
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ONERA The French Aerospace Lab hera motor test bench
Hera Motor Test Bench, 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
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ONERA The French Aerospace Lab aeroacoustic test bench b2a
Aeroacoustic Test Bench B2a, 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
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Average 90 stars, based on 1 article reviews
aeroacoustic test bench b2a - by Bioz Stars, 2026-08
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90
ONERA The French Aerospace Lab cryogenic liquid rocket engine test bench fault-tolerant control system
Cryogenic Liquid Rocket Engine Test Bench Fault Tolerant Control System, 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
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Average 90 stars, based on 1 article reviews
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90
ONERA The French Aerospace Lab demonstrator crash test
Demonstrator Crash 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
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Average 90 stars, based on 1 article reviews
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ONERA The French Aerospace Lab mercato test rig
Mercato Test Rig, 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
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EcoDesign Inc aerospace testing
Aerospace Testing, supplied by EcoDesign Inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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Average 90 stars, based on 1 article reviews
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ONERA The French Aerospace Lab m6 test case
M6 Test Case, 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
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ONERA The French Aerospace Lab aeroelasticity testing in a straight cascade wind tunnel
Aeroelasticity Testing In A Straight Cascade Wind Tunnel, 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
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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
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ONERA The French Aerospace Lab real data from the onera/cnes mascotte test bench
Schematic of novel aircraft featuring boundary layer ingesting <t>(BLI)</t> <t>ducted</t> fan propulsion systems.
Real Data From The Onera/Cnes Mascotte Test Bench, 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
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Average 90 stars, based on 1 article reviews
real data from the onera/cnes mascotte test bench - by Bioz Stars, 2026-08
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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: