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| Hanley Announces WingTail Calculator 2.0 |
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Posted Mon June 07, 2004 @11:06AM
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Hanley Innovations, a leader in aerodynamics
conceptual and preliminary design software, announces the availability of
WingTail Calculator 2.0 and WingTail Calculator Plus, 2.0.The Wing Tail
Calculator accurately computes lift, drag (vortex and profile) and moment
(about the center of gravity) for isolated airfoils, single wings or two-wing
systems (or keel-rudder interaction). It can also predict the neutral point
(or aerodynamic center) location and the angle of trim.
The WingTail Calculator uses the vortex lattice method (based on vortex rings)
for non-planar lifting surface analysis; a linear strength vortex panel methods
for airfoil analysis; a novel solution of the ordinary differential equation
form of the boundary layer equation for computing profile drag. The resulting
formulation naturally treats cambered, tapered and twisted surfaces. WingTail
can be used to solve problems related to wing and control surface sizing,
aerodynamics loading (lift & drag forces), cross section shapes (airfoils),
control surface placement and stability determination.
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