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4hv.org :: Forums :: General Science and Electronics
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Propeller Physics and VABs Program.

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Patrick
Wed Dec 31 2014, 10:01PM
Patrick Registered Member #2431 Joined: Tue Oct 13 2009, 09:47PM
Location: Chico, CA. USA
Posts: 5639
Im study your work Andy, and appreaciate it. im getting ready to get s-faced here shortly, sa the pre-requiste 2015 arrival.
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Ash Small
Wed Dec 31 2014, 10:11PM
Ash Small Registered Member #3414 Joined: Sun Nov 14 2010, 05:05PM
Location: UK
Posts: 4245
Patrick wrote ...

Im study your work Andy, and appreaciate it. im getting ready to get s-faced here shortly, sa the pre-requiste 2015 arrival.

I've had a look at Andy's work too Patrick, and from what I can gather, he's assuming a much higher disc loading than we've discussed. At least, that's my impression.

I suggest we consider how much CF we need for hover, then add extra for max thrust, say twice the hover figure, then add a safety margin, so we're looking at, say, three times the CF needed for forces at hover.

Maybe we need more than this, but it sounds about right for a 'starting figure'.

We'll be celebrating here too in a couple of hours.
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Patrick
Wed Dec 31 2014, 10:26PM
Patrick Registered Member #2431 Joined: Tue Oct 13 2009, 09:47PM
Location: Chico, CA. USA
Posts: 5639
ive got 3k fabric of the CF, so 4 to 6 layers of fiberglass and CF should be good.

though wed taper it at the tip, and thicken towards the hub.
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Andy
Thu Jan 01 2015, 01:08AM
Andy Registered Member #4266 Joined: Fri Dec 16 2011, 03:15AM
Location:
Posts: 874
Happy new year.
The top view can be adjusted, at present a value of 3.1 is the front force with .11 the back force or drag, instead of 20,20, 20,10 can be used which would make it smaller, the data is based on no torque adjust might and only 1 degree eff out of 90, still trying to work out the overall eff.
The data is assuming that drag has the opposite but equal force as lift,.
My design just has more sodility, any way I need to do some mediation on the matter, latter
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Patrick
Thu Jan 01 2015, 06:18AM
Patrick Registered Member #2431 Joined: Tue Oct 13 2009, 09:47PM
Location: Chico, CA. USA
Posts: 5639
WOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOOO OOOOOOOOOOOOOOOO, 2015 -- Tipsy !










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Ash Small
Thu Jan 01 2015, 01:41PM
Ash Small Registered Member #3414 Joined: Sun Nov 14 2010, 05:05PM
Location: UK
Posts: 4245
Even if it's thicker near the hub and thinner at the tip, the lowest drag figures will be obtained using just enough uni-directional carbon to give the strength we calculate is required.

Using more carbon than is actually required just increases drag and rotating mass.

We can adjust the angle of attack to give the required Cl from the tip to as close to the hub as possible, without Cd becoming too high.
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Patrick
Fri Jan 02 2015, 12:13AM
Patrick Registered Member #2431 Joined: Tue Oct 13 2009, 09:47PM
Location: Chico, CA. USA
Posts: 5639
ok so, unidirectional mostly extending from tip to tip, only clad with 1k on the bottom and then on top.
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Ash Small
Fri Jan 02 2015, 12:23AM
Ash Small Registered Member #3414 Joined: Sun Nov 14 2010, 05:05PM
Location: UK
Posts: 4245
Patrick wrote ...

ok so, unidirectional mostly extending from tip to tip, only clad with 1k on the bottom and then on top.

Well, the less carbon we use the less the drag. We do need a reasonable safety margin though, we don't want carbon shrapnel at Mach speeds wink
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Patrick
Sun Jan 04 2015, 03:57AM
Patrick Registered Member #2431 Joined: Tue Oct 13 2009, 09:47PM
Location: Chico, CA. USA
Posts: 5639
Uni-carbon...
1420343859 2431 FT167327 Uni


This carbon i layed up is 1k carbon, medium modulus, unidirectional. i can put these together and tailor the thickness in 0.004" layers. The cross pattern is an ultra-thin nylon mesh to keep it in all parrallel while wet.
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Ash Small
Sun Jan 04 2015, 06:20AM
Ash Small Registered Member #3414 Joined: Sun Nov 14 2010, 05:05PM
Location: UK
Posts: 4245
Patrick wrote ...

Uni-carbon...
1420343859 2431 FT167327 Uni


This carbon i layed up is 1k carbon, medium modulus, unidirectional. i can put these together and tailor the thickness in 0.004" layers. The cross pattern is an ultra-thin nylon mesh to keep it in all parrallel while wet.

Whether or not we want an external layer of cloth I'm not sure, but if we do, I assume it's best to wrap it around from the back of the blade, so there is a smooth layer over the leading edge.

We do need to do some maths here to determine how much carbon we need, and hence the CSA. (VABS may be useful here, if we have access to a 64 bit machine, or we could work it out the 'old fashioned' way, but I will need to revise the 'forces in a beam' thing and look up the strength of the particular CF we are using.)

XFOIL uses the chord length and profile, so adjusting chord length determines CSA for any NACA profile. (we will need a bit of maths as well, but for any NACA profile, the CSA is a function of chord length)

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