To give you precise values for the stability of Bee-wings,
we did some heavy-duty research with Andreas old wing in the laboratry of Tims
institute. Mounting the wing on a high tech test facility, we attached a fuselage-simulating-device
underneath it and slowly increased it's weight.
|
weight: 0 kg, deformation: 0 mm |
|
weight: 1.5 kg (equals an acceleraton of about 1.5 g), deformation: 0.5 mm |
|
weight: 3 kg (equals about 3.0 g), deformation: 0.75 mm |
|
weight: 4.1 kg (equals about 4.1 g), deformation: 1 mm |
|
weight: 5.1 kg (equals about 5.1 g), deformation: 1.2 mm |
|
first deformations in the aft part of the covering can be seen |
|
weight: 6.3 kg (equals about 6.3 g), deformation: 2 mm |
|
weight: 7.8 kg (equals about 7.8 g), deformation: 2.8 mm |
|
weight: 10.5 kg (equals about 10.5 g), deformation: 3 mm |
|
with this weight, deformations in the nose-part appear |
|
weight: 12 kg (equals about 12 g), deformation: 4.2 mm |
|
weight: 15 kg (equals about 15 g), deformation: 35 mm |
|
at this point the leading edge-section collapses, the main spar survives, maybe
the Bee could still fly, so we go on with increasing the weight... |
|
weight: 19 kg (equals about 19 g!!!), deformation: 35 mm |
|
weight: 22 kg (equals about 22 g), even the main spar collapses |
|
this severe destruction leaves no possibility of the Bee to keep airborne |
|
Out of this precise part of scientific research, we evaluated the following
deformation-to-force diagram: |
Next to this destructive work we did some towing tests with
the wingtip. This is for the fellow Water-Bee flyers. It gives precise information
to predict the behaviour of your Bee in case you are hit by a turbulence while
takeoff or landing and your wingtip touches the surface.
To all the children: Don't do this at home. The tests have all been done by
specialists wearing the right protective clothing and working according to the
well known IBWTR (International Bee Wing Testing Rules). Doing this at home can
cause severe damage to your carpet or flooding your livingroom.