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Maybe pop back and see Dave again you never know he may even give you a smile ,They were indeed fitted at different times by different people. The original panel which is still up there was fitted by Dave Newell about 8 years ago. The missing panel was added a couple of years later by a company that were fitting them at one of the Warner shows.
When I find a company to fit a new one I will get them to check the fixing of the other panel. As I mentioned in my original post everything seemed fine at Easter when a friend cleaned the roof for me!
Yes it was across the front of the roof.
What is the consensus of opinion regarding fitting a flexi panel instead - would it be more secure as the profile would be a lot thinner?
It's your eyes gov, on one the cable has been pulled out of the plug and the other one the cable has been ripped in half.But looking at it the connector seemed to be unplugged rather than ripped off but lets hope you get it sorted quickly and cheaply , is your solar still working
according to Specsavers my eyes are fine maybe the quality of my screen as I cant zoom in so I can see a plug thingy on the end of the one cable I'm not wrong but will stand corrected and bow to your greater knowledge photos on screens I dont seem to be able to see the detail other canIt's your eyes gov, on one the cable has been pulled out of the plug and the other one the cable has been ripped in half.
Panel defiantly went AWOL on the move.
Aerodynamics is definitely very weird and by no means intuitive. Most of the lift of an aeroplane wing is because of the curved upper surface, not the push from the tilted lower surface. There will have been a very strong uplift force due to the pressure difference between the air above and below the panel. Google Bernoulli Effect for further details.t is at the front.I'm amazed that it has missed both roof lights & the aerial?
Aerodynamics is definitely very weird and by no means intuitive. Most of the lift of an aeroplane wing is because of the curved upper surface, not the push from the tilted lower surface. There will have been a very strong uplift force due to the pressure difference between the air above and below the panel. Google Bernoulli Effect for further details.
Paradoxically, any turbulence or wind buffeting doesn't increase the upward force, it actually reduces it. The position at the front of the MH, as the air curves up from the front, is about the worst position for this pressure uplift effect.
A full width support across the front of the panel, acting as a spoiler, doesn't actually reduce the pressure uplift force either. But at least it provides more surface area for the adhesive. Adhesive strength depends on the total area of adhesive.
If the full width support reduces the flow underneath, then isn't that increasing the speed differential, and therefore increasing the lift force? As I said, not very intuitive, which is why they do so much wind tunnel testing to check the hand-waving arguments.In its most basic translation Lift is dependant on the speed differential of a fluid between the upper surface and lower surface of an object. Therefore the position at the front of the van is irrelevant in terms of lift, it just changes the angle of attack, probably past stall angle. Also putting a full width support across the front would have an effect as it would reduce the flow underneath the panel.
Put simply, No it will not increase lift.If the full width support reduces the flow underneath, then isn't that increasing the speed differential, and therefore increasing the lift force?
You're all making me paranoid! Our panel at the front is mounted widest side to the front although it does have the longer full width mounts on the shorter sides. It's been on for 3.5 years and when I cleaned it earlier this week it showed no sign of any movement or deterioration of the sealant so hopefully won't go for a fly!
In its most basic translation Lift is dependant on the speed differential of a fluid between the upper surface and lower surface of an object.
If the full width support reduces the flow underneath, then isn't that increasing the speed differential, and therefore increasing the lift force?
Put simply, No it will not increase lift.
Cal54, her panel went pasta also.Blinking heck this is getting very technical , I don think my van will go fast enough to take off and I thought Bernoulli was pasta
I have questions
RedFrame your first quote above seemed correct to me.
autorouter the same thought occurred to me, although I would rather have the blocker.
RedFrame your last quote directly contradicts your first quote and contradicts what I understand to be true?
If the front of the panel is blocked there is still lift as I understand it.
I am not an expert in this, but did do basic physics. My understanding is that laminar flow is not required for lift only a difference in pressure. Laminar flow is an advantage as it reduces drag and therefore increases efficiency. But it is not required.I can't explain 5 years education in one post, but in order to create lift the flow needs to be laminar. Imagine two molecules at the leading edge of a wing, one goes over it, the other under it. The two molecules must meet at the trailing edge of the wing and to do this they need laminar flow, simply reducing flow won't increase lift.
Cheers
Red
CorrectAnd bottom line the OP's panel wasn't stuck down properly.
Just been out and checked the security of my panel which I fixed with Sikaflex. Seems completely stuck. I think I'll add it to my trip check list to check it every time I go away.
I think the amount of lift will also depend on the angle of attack. I think a lot assume as it's flat on the roof there's no angle of attack but it depends on the direction of the airflow which could well not be parallel to the roof as it's just come over the windscreen. I recon if you put a flat sheet of ply on a roof rack there would be quite likely be lift although the ply is flat and as soon as the front becomes lifted there will be a huge increase as the angle of attack increases.I just did a quick experiment to test a hypothesis.
If there is no air under the surface and air flows above the surface you would suspect extremely high lift. But this is not the case. I wanted to test what would happen if you sealed all 4 sides of a solar panel (not advisable)
I placed a sheet of paper on my kitchen work surface and blew across it. No lift was generated.
When I bent the paper a little so that there was a gap under it, lift was generated when I blew.
So there needs to be air under and over. The air flow doesn't need to be laminar, and there doesn't need to be airflow underneath the surface.
Finally the surface does not need to be curved, although that appears to help.
Think that may just be due to direct pressure rather than aerodynamic lift?I think the amount of lift will also depend on the angle of attack. I think a lot assume as it's flat on the roof there's no angle of attack but it depends on the direction of the airflow which could well not be parallel to the roof as it's just come over the windscreen. I recon if you put a flat sheet of ply on a roof rack there would be quite likely be lift although the ply is flat and as soon as the front becomes lifted there will be a huge increase as the angle of attack increases.
A lot of glider wings make use of laminar flow and incorporate turbulator tape to control where the laminar flow detaches from the wing surface.Ahh so it may be the coanda effect causing the lift on my paper. I just checked and no lift is created if the paper is flat and parallel to the work surface.
But now I am thinking maybe there is some vacuum being formed by the paper being lifted up when placed flat on the surface. Experiments are over for today.
If anyone else fancies joining in