Computational Fluid Dynamics Lab

NACA 5-series airfoil at Re=300,000 and 15deg angle of attack. Iso-surfaces of Q=1.

NACA 5-series airfoil at Re=300,000 and 15deg angle of attack. Iso-surfaces of Q=1.

 Andreas Gross

Mechanical and Aerospace Engineering Department, New Mexico State University, Las Cruces, NM 88003

(575) 646-6179

 agross@nmsu.edu

Team Members

CFD Research

Applied Aero Research

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