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1987•NASA Technical Reports Server (NASA)Open access

An experimental low Reynolds number comparison of a Wortmann FX67-K170 airfoil, a NACA 0012 airfoil and a NACA 64-210 airfoil in simulated heavy rain

Anthony P Craig, R. John Hansman

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Abstract

Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1987

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Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1987

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OpenAlex reports 1 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1987

Key concepts: Airfoil, NACA airfoil, Relative wind, Angle of attack, Boundary layer, Reynolds number, Aerodynamics, Lift coefficient

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An experimental low Reynolds number comparison of a Wortmann FX67-K170 airfoil, a NACA 0012 airfoil and a NACA 64-210 airfoil in simulated heavy rain — Research Paper | ScholarLens