US: 2-engine Davis Wing Bomber

gjs238

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Was the Davis Wing ever used or considered for a 2-engined bomber?
How about a medium bomber?
How would a "Mini-24" have compared to the B-25, B-26 and others?
 
The Davis wing was used on th Consolidated XP4Y, a 2 engined flying boat, that could carry a prertty good bomb load also, but only 1 was built.
It used the same engine as the B-29, not enough to spare for the P4Y, so it was cancelled.
 
Last sentence from A wiki entry on the Davis wing.

"As speeds of aircraft of all sorts increased, the Davis wing's low low-speed drag could not make up for its higher high-speed drag, and use effectively ended."

Drag is not simple and what works well at low speed may not work at high speed ( Hawker Hurricane and Typhoon?)

where the crossover point for the Davis wing is I don't know. Davis wings are also pretty high aspect ratio. some good comes from this and somethings not so good.
 
Last sentence from A wiki entry on the Davis wing.

"As speeds of aircraft of all sorts increased, the Davis wing's low low-speed drag could not make up for its higher high-speed drag, and use effectively ended."

Drag is not simple and what works well at low speed may not work at high speed ( Hawker Hurricane and Typhoon?)

where the crossover point for the Davis wing is I don't know. Davis wings are also pretty high aspect ratio. some good comes from this and somethings not so good.

SR - you are right about that (I.E Clark Y on B-17 would not be useful on P-51. Having said that compressibility drag starts at about .3 (extremely negligible) and increases till .5 where it has a couple % increase to .6-.68 where there are smal localized drag divergence initiations (P-38 comes to mind). I don't feel that 'drag' would have been an issue with Davis airfoils for WWII 1943-145 model medium bombers.

Short answer - I don't know.
 
Didn't the B-29 have a Davis wing?

The B-29 used Boeing's Model 117 laminar airfoil, the wing featured the unusually high aspect ratio (wing span divided by mean chord) of 11, a detail that contributed greatly to reducing drag and increasing range.
 

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