![]() I have it in a JPG but can't put that here. The test pilot attributed this, not to the presence of a hole in the LE as suggested earlier, but rather the pilot positioned over the wing disrupting the flow at the center, most important section of the wing."įlair 30 scematics and spec's. He stated the test pilot felt the glide ratio and sink rate was quite poor, worse actually than modern flex wings. The label 'Designed by A-I-R reflects our. ![]() The team has amassed three decades of accumulated experience in hang glider production. By control reversal, it might have been meant that the downward-pitching effect of sudden flap deployment overrode the pitch-up of the elevons, rather than the usual kind of control reversal that afflict hang glider pilots flying sailplanes, or vice versa.īrett Snellgrove wrote in November 2005: "I received an email from an associate of the Flair 30 test pilot. (AERONAUTIC INNOVATION RÜHLE) Felix Rühle and his partners have a remarkable company which designs, developes and produces the highest performance rigid wing hang gliders available. Control reversal was suspected but unproved. After extensive test flights, including more than 50 hours logged by test pilot Knut Von Hentig, the prototype was destroyed in a crash at a sailplane club, when the sailplane pilot flying it dove into the ground at high speed from less than 100 m. The pilot could launch by foot, then lay prone in a special harness, and finally land on a skid. Design adopted from Impact Rigid wing (by its designer permission) Flaps and ailerons with torsion spar and. If weight will be an issue, a plain aluminum or even carbon tubing can be used, streamlined with styrofoam inserts and covered with plastic film. "The Flair 30 was a follow-up to the Flair design also developed by Günter Rochelt in 1987. They are streamlined and made from off shelve Hang Glider A frame uprights tubing. Text coming from Rigid Wing Models website :
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