FallingPhoenix said:
Okay, I can see that. Then again, like was said earlier, if you showed certain modern aircraft to an aeronautics engineer from the 1910s, I have a feeling they'd think you were ridiculous, given the design constraints, and I think that's where phavoc was coming from.
Let’s have a look at that. Let’s kidnap Glenn Curtiss, and have him knock some plane ideas around, before we show him an F-22.
We tell him the performance requirements we want, ask him to design a plane that meets those requirements according to the physics that he knows, and see what we get.
Well, one thing he
doesn’t know is the Whitcomb Area Rule, as that relates to supersonic aircraft; by extension, he doesn’t know about laminar flow, or even about the sound barrier, and associated shockwaves; he won’t even know about NACA’s research into airfoils. But he
will know it has to have a narrow cross-section, that the wings won’t need to be particularly big to provide the necessary lift (and if they were bigger they would be more prone to breaking), and that it would be stronger, and much heavier, than he would be used to, and probably, somehow, made of lots of aluminum. He would
also know that no engine he’s ever seen could run it, and that it would probably require quite a bit of mechanical engineering to have the required structural integrity, and may even need some materials in places he doesn’t know of.
Would he then, upon seeing the F-22, have a lot of questions? You betcha. But would he have been in the completely wrong ballpark? No. He’d nod, and go, “That’s about right.”.
See, the overall cross-section is a function of the available thrust at the desired speed, because of drag. The wing area is a function of the lift at that speed. The shape of the wing is a function of the diminishing returns on rigidity the further out along a spar you get. And what is left is more a less a box through the middle that you want to have a narrow cross-section, so it would be really long.
Now, admittedly, his design would have some shortcomings due to those things that were scientific discoveries after we kidnapped him. But it would more accurately match a Bachelor’s Degree Aerospace Mechanical Engineer’s attempt than you originally thought.
But what about the Space Elevator? What remains to be discovered
there?
The Space Elevator problem is constrained by wind drag. Is there something we don’t know about wind drag we don’t know? Maybe, but probably not.
It’s
also constrained by orbital mechanics. Is there something we don’t know about orbital mechanics? Maybe, but probably not.
The
constraints on the problem are well-known. Just like Glenn Curtiss would have gotten the general shape right, in spite of not knowing how it would be powered, we can get certain general characteristics right, in spite of not knowing how to tether the thing to ground and space securely. Now, at this point, you might go, “But what about some awesome rigid super-material that has the required strengths? That would be a match for those fancy aerodynamics things that Curtiss didn’t know, right?”; well, then it would be some crazy big lever trying to wedge its way through the soft crust of the Earth; the mechanical complexity of the base would skyrocket. A flexible tether would just plain be easier. Those constraints the NASA engineers built their designs to exist
for a reason.