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Heat transfer measurements from a smooth NACA 0012 airfoil
Local convective heat transfer coefficients were measured from a smooth NACA 0012 airfoil having a chord length of 0.533 m. Flight data were taken for the smooth airfoil at Reynolds numbers based onExpand
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Ice shapes and the resulting drag increase for a NACA 0012 airfoil
Experimental measurements of the ice shapes and resulting drag increases were measured in the NASA-Lewis Icing Research Tunnel. The measurements were made over a large range of conditions (e.g.,Expand
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Measurement of local convective heat transfer coefficients from a smooth and roughened NACA-0012 airfoil - Flight test data
Wind tunnels typically have higher free stream turbulence levels than are found in flight. Turbulence intensity was measured to be 0.5 percent in the NASA Lewis Icing Research Tunnel (IRT) with theExpand
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Generalized molecular orbital calculations on transition-metal dioxygen complexes. Models for iron and cobalt porphyrins
Calculs MO ab initio et CI sur des complexes de Fe et CO avec des coordinats dioxygene, NH 3 (pour simuler l'imidazole) et porphine. Description du complexe de Co comme un complexe Co 3+ −O 2 − ,Expand
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Synthesis and Characterization of the Mn(II) Complex of [15]aneN5
The complex Mn[15]aneN5CIPF6 has been prepared by the reaction of MnCI2 [15]aneN5.3HPF6, and NaOH in water ([15]aneN5 is 1,4,7,10,13-pentaazacyclopentadecane). The complex is obtained as a whiteExpand
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