First today I would like to outline what I would like to see in this Blog.
For 50 years hang gliding has been suffering a protracted dark ages. The first dark age started in the 1930's when hang gliding was banned by the German glider clubs followed by the world. This dark age ended with the 1971 Lilienthal meet. A second dark age came about due to crashes with the Cronk Kite. The result was a ban on all rogallos except "Standard Rogallos" considered by many to be the prototype of the unsafe hang glider. Yet this was all we were allowed! For our own safety! The worst was the 3rd, now more than 43 years long, the ban on home crafted gliders. I was notified one day after the decision was made by the HGMA. No more kits, no more home made , if you can't launch with out an assist forget it ( amazingly if it's a rogallo and windy it's quite alright to have three people wire you but no one is to assist a fixed wing!) Today The EAA has an Ultralight Hall of Fame, but still to this day there is no EAA Hang Glider Hall of Fame. Hang Gliding has not allowed home building, and
we don't merit any hall of fame, because of those who have succeed in killing the hang glider inventor/craftsman. It should be noted that it was the manufactures who banned the home built hang glider $$$. Hang Gliding does not merit a place in The EAA sub halls of fame because
there has been no contributions to aircraft and flight science by the hang gliding home built community for 43 years now.If you are a supporter of keeping hang gliding in the Dark Ages take it somewhere where it is welcome, because it's not welcome here
Some believe that for hang gliding to accommodate home building it would need to create an EAA like infrastructure-if this is more your interest hop aboard! First thing would be peer review-so my fellow hang gliding enthusiasts(
my peers) let me spend some time on the airfoil I'm planning on for
your review.
The Quicksilver's original airfoil was so profile drag dominate that the aspect ratio difference of the QS B and QS C did not matter . One can raise the aspect ratio but it still gets the profile drag indicated 7 to 1. We have many better options. First the airfoil must be compatible with the membrane and batten wing. Second it must be high lift at low speed and low profile drag. Last it would be helpful if it was stall resistant. 4 airfoils come to mind-Alpine, Fledge 2 (Benedek B-6407-E mod) the Fledge 3, and the Kasper (NACA8-H-12 mod). If I had to make a single surface wing it would be The NACA8-H-12 that Kasper used. For a double surface I like the low speed characteristics of The Fledge 2 over the Alpine. I also feel that for batten installation, and good high speed without the need for 80% double surface I like the Fledge 2 over the 3.
Fledge 2 suffered from tip stall but it was due to flattening out the airfoil as it approached the tip. This came with high profile drag outboard and more induced drag as well. So my build will rum the airfoil 100% to the tip and then make use of wing tip enhancements.
- Airfoil.jpeg (116.54 KiB) Viewed 5571 times
In the top sketch I have given the geometric formula for the airfoil. In the middle sketch is a wing cross section at a compression strut. The lower drawing shows on top, the current state of the art in trailing edge, and below my up grade. Note the sever ramp on top, and on the bottom the mild tapper that leads into the trailing edge spar. To the rear of the spar on the bottom is an aluminum H channel section with a 3/8ths inch tube of aircraft aluminum stringer.
The H channel makes an excellent saddle on the 1 and1/8th inch rear spar as well as the 3/8ths. Note the low refractory angle past the rear spar in the tapper out. The 3/8ths radius is large enough to reduces chaffing of the fabric that a sharper edge would create. I hope to see the trailing edge modification create a TE as clean as the Fledge's. I'll know if the L/D hits 14 to 1.
The ribs or battens are planned on being the old fashion two piece wood type. They are wide, and flat on top not tubular.
The slack in the batten pockets will be on the underside only, thus making a flat plane on the top of the upper surface instead of ridges and sags. The main engineering questions here are: Will the wood battens insert readily, how to secure the batten, can I get away with more than 50% double surface, due to the holes in the pockets will I have ram inflation issues, or rip and tear issues. Note in the middle sketch, as one increase the amount of double surface the opening in the front pocket for the escape of the compression strut becomes longer and longer- what are the limits and will ballooning or strain become an issue? I'll be building a full scale wing section to help answer these questions and more. Well I'm going to stop here-I think I've used up my attachment allowance and this post is long enough. More latter.