Author Topic: Me-410 props?  (Read 1964 times)

Offline Charge

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Re: Me-410 props?
« Reply #30 on: August 24, 2011, 03:48:23 AM »
"Higher wing-loading doesn't mean less draggy."

So what is the point of putting small wings on a plane then? Cost?  ;)

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Offline PJ_Godzilla

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Re: Me-410 props?
« Reply #31 on: August 24, 2011, 04:07:07 AM »
"Higher wing-loading doesn't mean less draggy."

So what is the point of putting small wings on a plane then? Cost?  ;)

-C+

He prefaced the statement. Consider a barn door with F-104 wings, then consider a streamlined fuse with larger wings. Clearly, you could make a draggier ac with a higher wingloading. Generally, this does not obtain. I think Stoney's only point was that the wing is only one part of the overall drag picture.
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Offline Charge

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Re: Me-410 props?
« Reply #32 on: August 24, 2011, 07:27:48 AM »
Ok, with that I agree or course. I thought that as wing-loading  is calculated from wing-area to weight that would automatically mean that high wing-loading is caused by a small wing (or unnaturally great weight) and there is not really any sense to make a small wing except to counter parasitic drag, that is why the statement seemed a bit strange.

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Offline Krusty

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Re: Me-410 props?
« Reply #33 on: August 24, 2011, 10:05:40 AM »
As an interesting note, I recently found this on LEMB (clipped):

"There are figures for just this given in Mankau/Petrick, near the end of the book.

BK5 listed as 15kph penalty, 2x 3x WG21 : 20 kph. Abwurfanlange Mittelflugel - 4 x SC 50 od. 4 x BL-Bomben : 25 kph. Both 2x300L and 2x900L drop tank configurations : 25 kph."

The follow up asked if he meant 2x 2x or if that's the experimental 2x 3x drag.

Offline Stoney

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Re: Me-410 props?
« Reply #34 on: August 24, 2011, 12:20:34 PM »
Ok, with that I agree or course. I thought that as wing-loading  is calculated from wing-area to weight that would automatically mean that high wing-loading is caused by a small wing (or unnaturally great weight) and there is not really any sense to make a small wing except to counter parasitic drag, that is why the statement seemed a bit strange.

-C+

The original statement was that higher wing loading meant less drag.  If, for example (all other things being equal), the wing area remains the same size, but the weight doubled, the drag coefficient would be the same (i.e. the plane is just as "draggy"), but the wingloading would be much higher.  Without knowing what type of thrust/power the Me410 is capable of, we can't really make a comparison of how the higher wingloading will effect the plane, one way or the other.  If the higher wingloading was a result of a smaller wing only, then we could potentially say "less draggy".
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