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Zhi Yang

Post-Doctoral Researcher

Biography

NASA ULI Technical Sub-Group: Computational Methods & Analysis

NASA ULI Research: Task 1.02 Aero Structural-Acoustic Optimization of SNLF Wing Configuration; Task 2.02 Complete Design of an SNLF Wing

 

 


Research

Unsteady aeroelastic simulation methods as well as mesh curving techniques.


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