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Predicting Quadcopter Drone Noise Using the Lattice Boltzmann MethodThe market for new vertical takeoff and landing vehicles, including autonomous urban air taxis and drones for applications such as package delivery, imaging, and surveillance, is growing rapidly. However, aerodynamic noise continues to be the biggest roadblock to community acceptance and adoption. To predict the aerodynamic noise generated by an isolated quadcopter drone, derived from from first principles, we used the Lattice Boltzmann flow solver within NASA’s Launch Ascent and Vehicle Aerodynamics (LAVA) solver framework. The solver’s computational efficiency, and the complete absence of labor-intensive manual volume mesh generation in the workflow, are key to making routine aeroacoustic analysis of urban air taxis and drones from first principles possible.
Document ID
20200000627
Acquisition Source
Ames Research Center
Document Type
Poster
Authors
Cadieux, Francois
(Science and Technology Corp. Moffett Field, CA, United States)
Barad, Michael
(NASA Ames Research Center Moffett Field, CA, United States)
Jensen, James
(NASA Ames Research Center Moffett Field, CA, United States)
Kiris, Cetin
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
January 31, 2020
Publication Date
November 17, 2019
Subject Category
Acoustics
Report/Patent Number
ARC-E-DAA-TN77267
Meeting Information
Meeting: SC19 (The International Conference for high Performance Computing, Networking, Storage, and Analysis)
Location: Denver, CO
Country: United States
Start Date: November 17, 2019
End Date: November 22, 2019
Sponsors: Association for Computing Machinery, Institute of Electrical and Electronics Engineers (IEEE)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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