7480W

Could anyone please tell me the total height, width inside the wheels, and alxels to the bottom of the plane of the landing gear. If you could. Thank you so much for your time, TJ

Has anyone considered the possiablity of sweeping the main wings more to reduce drag. I know that with this the twist would have to be increased in order to not stall tips first. Maybe im being crazy here. One possibality with too much money and time the possibality of movable wings, so it could remain the same landing and low speed flight. If the wings were swept back far enough it could almost be a delta style wing. I know some very different principials, but it could help with the mach number problem, I was told that a greater swept wing with the same airfoil has a higher mach # usage, Though not from the most relaible sorce.I think that the cannard would have to be different as well to stop it from being the limiting factor. I think this will get really complex really quickly but, Just a thought. Thank You all for being so helpful as well all the great advice in this thread.

Has anyone had any experiance with this type of foam. I bought a sheet just to play with and it seems promising. Forms very well, Has no bubbles and an estimated density 1.5 lbs per Cubic Ft. Any thoghts or ideas is greatly appriciated. And if anyone knows what the technicnal differnece is that makes it 'Extruded' ? Thank you

Thanks for the advice, I am still at ground zero but at least I'm getting supplies together. I was planning on going with a different fuselage. But to what extent is still being kicked around. One of my friends said, why not? But maybe not the best idea. Any specifics on turbo plane's high altitude cruse speed? Thanks.

I was wondering has anyone over done a EZ using a turbo normalized O-320 and or one being pressurized. Any thoughts on this idea?