Konrad!We don’t like them for wing spars.
And while tubes are used for the manufacture of crane booms the cross section of the boom is normally triangular.
I will jump in and say that I find these exchanges stimulating. While I have a strong science background, I am not an engineer. I have a strong interest in learning all I can about the design, manufacturing, and flying of these planes and enjoy the discourse offered in this forum.In the smaller models I believe tube spars are used for ease of manufacture. Most designers don’t like them, as little of the fibers are actually placed where the mass is used to great effect.
The crane boom has to deal with very high loads in one direction and some much lighter side load. A tube offers resistance equally 360 degrees. The crane boom and maybe our tail boom don’t see loads equally (360 degrees). So the boom tries to put material where needed.
The round tail boom is good as we really don’t know how the boom will whip in a crash. But with another cross section we can try to define how the boom will fail.
I love them on the smaller models - Light, strong, easy to get, easy to use, many different fibre orientations available, spiral, straight, straight/wrapped etc, lots of wall thicknesses can be had, can take ballast, the joiner rods can be carbon, alumnium or steel etc.In the smaller models I believe tube spars are used for ease of manufacture. Most designers don’t like them, as little of the fibers are actually placed where the mass is used to great effect.
OK first I want to take back what I said originally - I was having a Doooohhh moment! In fact, most but not all crane booms are square in section and not triangular, though many are. As you say, round tubes offer the same load resistance for 360 dgrees, but in fact the loads and the stresses to be withstood in any direction are to a large extent designed in to the construction of the structure.The crane boom has to deal with very high loads in one direction and some much lighter side load. A tube offers resistance equally 360 degrees. The crane boom and maybe our tail boom don’t see loads equally (360 degrees). So the boom tries to put material where needed.
Aha - and there you have it. We are now blessed with two lovely variables to help us:The round tail boom is good as we really don’t know how the boom will whip in a crash. But with another cross section and lay up we can try to define how the boom will perform.
I think we all learn here. I certainly do.Thank you. I too learn a lot out of this kind of debate (exchange of ideas).
The new Spada fuselage is smaller in cross section than the FS I think. Its not even half of the cross sectional area of the MK1. And it follows the Heorner doctrine.One of the stiffer, lighter and proven more durable are the booms found on the Freestyler 5.
I don’t think it shows up well but the fuse is changing cross section from the non tapered straight sided rectangle adjacent to the wing to a nice triangular cross section with the apex at the top. This buts a lot of fiber on the bottom to deal with the left and right side loads of a typical bad landing ( my normal stuff).
I'll say it again: The new Spada fuelage cross section is smaller than the FS I think. Its not even half of the cross sectional area of the MK1.I’m really starting to like what I see structurally in the Freestyler.
Now if they understood what Schumann observed then I think they would have one of the greatest designed F3F racers. But as I don’t think Schumann, an amateur aerodynamicist, characterized what he observed. So maybe the spanwise flow from the tip to the root at or near the stall isn’t understood by many.
Now your wing on the Redshift handles this very well and is why your 18:1 aspect ratio wing works so well at high Cl numbers (turns) when others not so much.
Like I’ve said I love the wing, but the fuse not so much*. So unless there is a reason to keep the fuse cross sections similar to the mk1 I see room for improvement, both in aerodynamic and structural geometries.
The same shoulder fillets are still there on the new Spada.*one big plus I see in the mk1 fuse are those shoulder fillets at the wing LE. I know that’s have saved my wrecks from the wing totally crushing the fuse in that area.
This is a bit of an anomaly. It used to be that the (actual)cost of making a model in E-Europe was more than that in China, and by a fair amount. Thats no longer true. Prices for the models from China have risen, though the large proportion has been due to materials price rises.Now it needs to be said that the price of the RedShift was a little over Half that of the Freestyler 5.
I'm your Doctor, so on these things - trust me.So watts and all I loved the Redshift enough to own 3. In fact one has just risen from the dead! Working the radio set up right now.
View attachment 12380View attachment 12381
A rose by any other name would smell as sweet. My appoligies to Bill...
Spada will be a fast, high-end 3M sports model. The fact that it will be pretty competitive in F3f is purely cooincidental.
...
Doc.
Surpise surprise! Konrad, I have been telling you this for a couple of days - what are you on? I want some!Well, well, well, it looks like Strega is compliant with my understanding of Hoerner’s reduction of junction drag discussions.
No. I have given enough information here, Konrad and anyway that would need a bunch of special views made.Frontal area looks good. Can you post cross sectional views of the fuselage all along the wing to fuse junction?
Yep.I'm starting another thread called the Good the Bad and the Ugly. As I think we have beaten this horse junction drag to death in this thread.
Hum, all the tower cranes swinging wildly over the city have triangular cross sections booms. The side load that I was thinking of that might mimic the side load of a whipping tail boom is the force needed to swing the heavy load over a spot.OK first I want to take back what I said originally - I was having a Doooohhh moment! In fact, most but not all crane booms are square in section and not triangular, though many are. As you say, round tubes offer the same load resistance for 360 dgrees, but in fact the loads and the stresses to be withstood in any direction are to a large extent designed in to the construction of the structure.
There will always be that one time where for some reason the structure exceeds its design limit and fails and this is because the crane boom does NOT see the loads equally.
Its designed to lift loads from the deck up, against gravity,more or less in one direction only and apart from any unplanned side or other forces, thats what it does.
....
Cheers,
Doc.
Actually my recent files have been done using Onshape, no Catia for a couple of years.Isn't that the power of CAD? Wth a 3D model you can generate cross sections all day long by defining the plane pass through (about 3 mouse clicks in Catia v5).
(Now I haven't used Catia in over 20 year so I might be off on the click count).
Can’t let the Catia out of the bag!Actually my recent files have been done using Onshape, no Catia for a couple of years.
There is a limit to how much information can be given away prior to the model actually coming out.
This crosses it.
Cheers,
Doc.