In this space I would first like to introduce my Quicksilver project, and then start a dialog about my design issues.
The Quicksilver-II project will have 4 phases, and terminate, if it runs to it's full conclusion in an electric self launch, self recovering motor glider. The project starts with the creation of the Quicksilver-II HG (Hang Glider) then this is the wing to which a trike is attached to create a primary tow glider (PTG). How much weight I will have to work with (up to150lbs max) will determine the third phase-adding fairings to create a secondary tow glider (STG). Once then ready I'll add the motor. Right now we will focus on the hang glider.
The hang glider from the start will be created with the end MG ( Motor Glider) in mind. For instance, the HG root tube is a thin wall 1.5 inch tube, and the trike requires a 2 inch square tube. So I will use a 1 5/8th's thin wall tube and saddles, so my mating surfaces come to the same plane as a 2 inch square tube. When the time comes to add the landing gear, the 1 5/8ths will swap out to a 2 inch square with no other changes than bolt off, bolt on.
The HG's improved features over the original Quicksilver are,
1- A Fledge-II airfoil,
2- A trailing edge added to the rear spar,
3- A breakdown feature for the wing so it will fit in a standard tube bag,
4- Advanced wing tip enhancements.
Let me start with the wings breakdown feature. It consists of using U channel brackets to mount the compression struts to the spars. The LE spar's brackets have bolts that act as an axle. The TE spar's brackets have pins that come out to allow the struts to fold along the leading edge. Then the TE is moved along side the LE, the bundle is tied and the wing goes in a standard tube bag. See Sketch. The brackets are 1/8 in thick 6063 T5 with saddles in between the spars and the base of each bracket. The bolts are 1/4 AN4 the pins are 1/4 clevis. Now here comes the tricky part, the gap in each bracket is 1 inch. I feel I need to run a less than 1 inch in diameter compression strut so to be able to place a sacrificial nylon washer in between the strut tube and the bracket. It may be also best to place a nylon or other material collar on the pin end of the strut. 7/8ths inch tube is not cost effective or weight effective. 3/4 has two wall thicknesses that may work and are cost and weight effective. If I use 3/4 inch I can put nylon collars on each end of the strut and when they get chewed up replace the collar.
The standard strut is 1 inch by .049 wall, the options are 3/4 by .058, or 3/4 by .065. Will either or bolth have the compression strength to meet or exceed the standard tube. I know that if the wall thickness remains the same, the cross section area determines the relative strength in compression. Ergo .5 squared x Pi vs. 3/8ths squared x Pi. but I am at a loss to figure the wall thickness contribution. So I could use some help on this computation.
If you, the reader have the math and science knowledge in these areas please chime in. In fact as I go through the plans anything you may see as an error, or have a better proposal chime in. Negative criticism should be constructive negative criticism.
Some basic details of the Quicksilver-II HG. Span 34' cord 4' 3" AR8 Tail group, standard Quicksilver MX less the elevator. Airfoil is Fledgling-IIB root section. Wings have spolierons, the estimated L/D is 14 to 1 and the minimum sink about 120'/min. The wing tips are Quicksilver Ultalight pressure gate with droop tip from the upper edge of the cord downward. Above the cord top the forward section is a Kasper pressure gate and the rear is a plano convex winglet. The top enhancements are optional so in the early phase of practice the stall and tip inertia can be minimized.
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Ruined a perfectly good buzz