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Design of a natural laminar flow airfoil for the light transport aircraft
Authors:K. R. Srilatha  G. S. Dwarakanath  P. Ramamoorthy
Affiliation:(1) Present address: Computational and Theoretical Fluid Dynamics Division, National Aeronautical Laboratory, 560017 Bangalore, India
Abstract:Summary As a substitute to the NASA GA(W)-2 airfoil, that is envisaged for a Light Transport Aircraft (LTA), a new airfoil NAL-MSNLF-136 is designed at NAL. It is shown according to model calculations that the thicker NAL airfoil shows better aerodynamic efficiency than the GA(W)-2 profile in the operatingCLrange.
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