Just watched a video of the first successful taxi tests of what some are calling the largest airplane in the world. I'm no engineer, but that thing looks scary. It's designed along the same lines as the airplane that will carry the sub orbital rocket that Scaled Composite's has designed. What I don't understand is the only attachment point between essentially two different airplanes is the wing. There's no attachment at the horizontal. How can the wing handle the twisting, differences in yawing and even differences in thrust load between the left side engines and right side engines. Amazing that "center section" of wing will be able to withstand these loads for an extended period of time.
What do you think?
Any engineers on here that can maybe explain this to me?
Thanks
Brian+
What do you think?
Any engineers on here that can maybe explain this to me?
Thanks
Brian+
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