Yea this thing was HUGE.
The cannards at the front had a span of 40m, with 80m span wings, and 80m long, 700 ton flying in the air, now i am all for natural progression and all that but hm kinda worrying
Have just completed a project at uni, the brief being to desgin a 1000 seater aircraft still within the JAR regs.
We used 3 LS on our desgin, prooved very helpful in the CofG calcs as was able to put more weight up front which helped with the CofG margin, and we planned to use fuel triming...
Hello all,
New to this site, i am currently at uni studying Aerospace Engineering.
I am doing a project using a CFD package, (PHOENICS) which will only give me pressure and velocity values at points. But i need to work out how much lift the shape is creating, i have undergone the pain staking...