Fri Nov 02, 2012 6:58 pm
Fri Nov 02, 2012 7:34 pm
Sat Nov 03, 2012 11:38 am
Sat Nov 03, 2012 5:46 pm
Sat Nov 03, 2012 6:24 pm
Mark Allen M wrote:
North American XF-82 44-83886(?) with 445-gallon droppable tank 105-inch rockets 110-gallon tank and a chemical tank
Sat Nov 03, 2012 9:20 pm
TriangleP wrote:I was curious about what the technical reason was that inward rotating props didn't work...found this info online posted by SoD Stitch on WW2aircraft.net.Warren M. Bodie, in his book The Lockheed P-38 Lightning: The Definitive Story Of Lockheed's P-38 Fighter, states that, "Engine rotation was changed so that the propellers rotated outboard (at the top), thereby eliminating or at least reducing the downwash onto the wing centersection/fuselage juncture. There was, by then, no doubt that the disturbed airflow, trapped between the two booms, was having an adverse effect on the horizontal stabilizer. No problem was encountered in reversing propeller rotation direction; they merely had to interchange the left and right engines."
I suppose the same problem existed for the XP-82, as it has twin booms and a large horizontal tail as well and inward rotating props threw the propwash onto these surfaces. Is it me or do these engines in this headon photo look like they've been already swapped? Anyway, so the engines were swapped on the XP-82 as DanK wrote. Maybe this reason has been posted on WIX before, apologies if this be the case...