- Main beam at about 1/4 of the chord.
Reasoning: Aerodynamic load bends the wing up but does not twist the wing. Reasonable upward bend hardly affects lift. So light weight construction can be chosen. - No sweep.
Reasoning: Aerodynamic load on a swept wing introduces strong twisting moments. Straight wings are more efficient than swept wings. Straight wings can do without a spar. - Pitch unstable configuration.
Reasoning: The traditional means to achieve pitch stability necessarily compromise efficiency (tail planes, canards, twisted swept wings, or airfoils with positive Cm) There is a reason why all birds fly severely pitch unstable configurations. Proposed solution: Achieve stability by lateral movement of the pilot relative to the wing. This adjustment of the centre of mass is analogous to steering a bicycle. - Attach the pilot to the wing rather than hang him a metre below.
Reasoning: The attached pilot gets a much more immediate feel for the current angular movements of the wing. This is a prerequisite to reliable pitch control by weight shift. - Decent positive dihedral.
Reasoning: Dihedral induces both, roll stability and directional stability. - Initiate turns by wing warping combined with drag devices at the tip.
Reasoning: Wing warping is the most efficient way to induce differential lift. A straight wing is easy to warp at the root. Unfortunately, differential lift also induces adverse yaw. Bird of prey compensate with counter rotation of their fairly large tail. Sea birds soar without engaging their tail. They use the instability of the anhedral of hanging wings. Asking the pilot to dynamically control unstable pitch is already a tough call. The sea birds way is probably not feasible for humans. A large flat tail like the falcon of this forum adds more mechanical complexity than I like. In addition, the tail might stall and induce "interesting" manoeuvres. Drag devices at the tip may not be the most efficient way to counter averse yaw. But they are reliable from a control point of view. - Use cheap, mass produced materials.
Reasoning: I'd like to build my wing without a NASA scale budget. Compared to the 1960s we have access to a few more light weight materials. In particular, I feel, the potential of polymer foam has not yet been explored for hang gliding. - Use feathers rather than a sail.
Reasoning: Birds beat pterosaurs and bats in the game called evolution. Seriously, feathers are modular, easy to replace when broken. Bird type wings do not apply bending loads to their bones. Other than the actual lift, feathers don't pull on the spars, errm, bones. The big challenge is of course, to construct man made equivalents to bird feathers scaled up by about an order of magnitude. Currently, I am in favour of XPS foam layered between sheets of BoPET with a shaft made of a regular carbon tube. Experiments will have to show if this is viable.
---<)kaimartin(>---
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