Velocity distributions on arbitrary airfoils in closed tunnels by conformal mapping
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AIR FLOW - AIRFOILS, ARBITRARY 2-DIMENSIONAL↗
Engineering topics
Moses, H E
Publications and source records attributed to Moses, H E.
Velocity distribution on symmetrical airfoils in closed tunnels by conformal mapping
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WIND TUNNEL TESTS - CORRECTIONS↗
Velocity distributions on two-dimensional wing-duct inlets by conformal mapping
The conformal-mapping method of the Cartesian mapping function is applied to the determination of the velocity distribution on arbitrary two-dimensional duct-inlet shapes such as are used in wing installations. An idealized form of the actual wing-duct inlet is analyzed. The effects of leading edge stagger, inlet-velocity ratio, and section lift coefficients on the velocity distribution are included in the analysis. Numerical examples are given and, in part, compared with experimental data.
Perl, W↗
Velocity distributions on two-dimensional wing-duct inlets by conformal mapping
Explore the source record for details and available documents.
Perl, W↗
Velocity distributions on arbitrary airfoils in closed tunnels by conformal mapping
Explore the source record for details and available documents.
Moses, H E↗