mrblucor
Mar 29, 2008, 02:01 PM
Hello everyone,
I've been looking through this thread and some of the links. What I have found are discussions on specific airfoils and some basic airfoil design information. I'm looking for some practical tips on getting more from ARF's and scratch builts. I'm an engineer but not an aeronautical engineer. I'm looking to get the biggest bang for the buck. I don't want to spend all winter working on a foamy to try to make it perfect. I want to direct my efforts to the biggest problems first. If 5 minutes of sanding will make a noticable difference, then I'll do it. As my modeling skills have gotten better with time, I've done things to my models that are not in the instructions. I hope my efforts are not a waste of time. Here are some of the situations I've encountered and what I've done. I consider you guys to be much more knowledgable than me. I welcome your comments and input.
Shumante F-18: This plane is built of flat foam. I rounded the leading edges and tapered the trailing edges to a fine point. This seems to make the plane go faster and glide longer. Less drag. I've seen guys leave the trailing edge flat. Isn't this a no no? I've also been told not to sand the leading edge to a point because this will cause the wing to hunt. Is this true? After a few flights, I taped the flying surfaces. This made the them smooth and stiff. The plane flew much better after this. I'm not sure if it was because the wings were stiffer or beacuse they were smoother. It is possible that there was some undetected flutter that was solved by the tape. The tape is a lot smoother than the foam, this could mean less drag. On my second F-18, I did all the above plus made the fuse smaller, omitted the canopy, and smoothed the fuse as much as possible. This plane was a fantastic flyer. It also came in an ounce or two lighter than the first one. I figure decreasing the cross sectional area of the fuse has got to decrease drag. It might be that the ounce or so less weight had more to do with its flying characteristics than the smaller fuse. I went head to head with another F-18. Same motor/prop/battery, his came in at 18 oz and mine at 16 oz. He had it painted which left a semi rough surface, better than raw foam but not as smooth as the tape. he also had squared trailing edges. Mine flew faster, slower, and longer per charge. I'm thinking weight, trailing edges, and smoothness were the difference in that order. Does that sound right? What do you think was the biggest factor? Did I get the importance of each factor right?
I've also been toying with the idea of installing a fillet where the wing meets the fuse. I've been told that right angles cause drag. Would this be worth doing? Would some foam triangle stock work OK? does the fillet need to be exactly shaped to make a difference? How about a simple airfoil shape to the wings. Is this more trouble and weight than it's worth?
EPS and EPP foam: Many ARF's are built of these two materials. The manufacturing process leaves moulding injection marks. The EPS foam has large round injection marks and the EPP planes have lots of small dimple like marks. Think GWS and Multiplex. These airplane generally have airfoil shaped wings and some even have a fillet where the wing meets the fuse. It seems to me that the injection marks add drag to the airframe. I sand down the peaks and fill the valleys. I think this is worth doing from a flight characteristic view. I have also tried sanding all the foam parts in an effort to make them smoother. I have no head to head flight data to say wether this is helpful or not. I believe it's worth doing.
I'm sure there are many things I've missed. I'm not trying to make a pylon racer or thermaling machine, I just want to try to get more from the average ARF or flat foam project. I think the comments generated from this could be put together and made into a top 10 list of things to do to improve typical preformance. This could also include weight reduction techniques and how a 5% reduction in weight applies to the flight characteristics of a model. It boils down to the question of wether it's worth doing or not. I know this is subjective. It would be nice to know if a proposed change will most likely make a noticable difference or not. All comments, suggestions, and data are welcome. Remember, I'm looking for simple things that will make the greatest difference.
Thanks in advance, JB
I've been looking through this thread and some of the links. What I have found are discussions on specific airfoils and some basic airfoil design information. I'm looking for some practical tips on getting more from ARF's and scratch builts. I'm an engineer but not an aeronautical engineer. I'm looking to get the biggest bang for the buck. I don't want to spend all winter working on a foamy to try to make it perfect. I want to direct my efforts to the biggest problems first. If 5 minutes of sanding will make a noticable difference, then I'll do it. As my modeling skills have gotten better with time, I've done things to my models that are not in the instructions. I hope my efforts are not a waste of time. Here are some of the situations I've encountered and what I've done. I consider you guys to be much more knowledgable than me. I welcome your comments and input.
Shumante F-18: This plane is built of flat foam. I rounded the leading edges and tapered the trailing edges to a fine point. This seems to make the plane go faster and glide longer. Less drag. I've seen guys leave the trailing edge flat. Isn't this a no no? I've also been told not to sand the leading edge to a point because this will cause the wing to hunt. Is this true? After a few flights, I taped the flying surfaces. This made the them smooth and stiff. The plane flew much better after this. I'm not sure if it was because the wings were stiffer or beacuse they were smoother. It is possible that there was some undetected flutter that was solved by the tape. The tape is a lot smoother than the foam, this could mean less drag. On my second F-18, I did all the above plus made the fuse smaller, omitted the canopy, and smoothed the fuse as much as possible. This plane was a fantastic flyer. It also came in an ounce or two lighter than the first one. I figure decreasing the cross sectional area of the fuse has got to decrease drag. It might be that the ounce or so less weight had more to do with its flying characteristics than the smaller fuse. I went head to head with another F-18. Same motor/prop/battery, his came in at 18 oz and mine at 16 oz. He had it painted which left a semi rough surface, better than raw foam but not as smooth as the tape. he also had squared trailing edges. Mine flew faster, slower, and longer per charge. I'm thinking weight, trailing edges, and smoothness were the difference in that order. Does that sound right? What do you think was the biggest factor? Did I get the importance of each factor right?
I've also been toying with the idea of installing a fillet where the wing meets the fuse. I've been told that right angles cause drag. Would this be worth doing? Would some foam triangle stock work OK? does the fillet need to be exactly shaped to make a difference? How about a simple airfoil shape to the wings. Is this more trouble and weight than it's worth?
EPS and EPP foam: Many ARF's are built of these two materials. The manufacturing process leaves moulding injection marks. The EPS foam has large round injection marks and the EPP planes have lots of small dimple like marks. Think GWS and Multiplex. These airplane generally have airfoil shaped wings and some even have a fillet where the wing meets the fuse. It seems to me that the injection marks add drag to the airframe. I sand down the peaks and fill the valleys. I think this is worth doing from a flight characteristic view. I have also tried sanding all the foam parts in an effort to make them smoother. I have no head to head flight data to say wether this is helpful or not. I believe it's worth doing.
I'm sure there are many things I've missed. I'm not trying to make a pylon racer or thermaling machine, I just want to try to get more from the average ARF or flat foam project. I think the comments generated from this could be put together and made into a top 10 list of things to do to improve typical preformance. This could also include weight reduction techniques and how a 5% reduction in weight applies to the flight characteristics of a model. It boils down to the question of wether it's worth doing or not. I know this is subjective. It would be nice to know if a proposed change will most likely make a noticable difference or not. All comments, suggestions, and data are welcome. Remember, I'm looking for simple things that will make the greatest difference.
Thanks in advance, JB