Affiliation:
1. Technion--Israel Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Reference43 articles.
1. High-Order Large Eddy Simulation and Immersed Boundary Method on Dynamic Meshes: Application to Rotorcraft Aerodynamics
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3. Ning, Z. “Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers,” Ph.D. thesis,Iowa State University, December 2018. URL https://lib.dr.iastate.edu/etd/16427/.
Cited by
2 articles.
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