phavoc said:
AN-225 - heaviest aircraft made to date (https://en.wikipedia.org/wiki/Antonov_An-225_Mriya).
Yes, agreed, this shows that 600 tonne aircraft can fly. It does not at all show that 6000 tonne aircraft can't fly.
phavoc said:
The Type-R is 10.5 m wide, 6 m high and 51 m long. At it's widest the craft is 27 m (wing tip to wing tip) - from the MGTv2 deckplan.
Well, the lower deck is double height, so the internal height is about 9 m, or perhaps 10 m externally.
phavoc said:
Scale from illustrations of the Type-R are varied. A simple sample will show this, but all we have are various illustrations and not actual ones from reality ...
I agree completely. We have many illustrations of the same craft that don't agree with each other. So which is the correct one with the correct dimensions?
phavoc said:
Type-R is 4,000 tons. We don't know the thrust capacity of the Type-R.
We know it can achieve a nominal acceleration of 1 g ≈ 10 m/s², so it must have a thrust of about 40 MN. Quite a bit more than the roughly 1.4 MN of an An-225.
phavoc said:
If you can provide me the type of airfoil and angle of attack I can plug the rest in.
You have claimed that it can't possibly fly, since you can immediately see what the aerodynamic properties of the wing are, so you tell me? Or simply show that it can't possibly fly with any possible wing profile.
I have no idea what the properties would be, and can absolutely not estimate them from a hand drawing.
And I guess that William H. Keith, Jr, who, I believe, draw the original Subbie illustration and deckplan didn't calculate, or even bother considering, the lift coefficient either.
phavoc said:
Even you ( I would hope) would have to agree the Type-R wing is not at all efficient compared to any known aircraft. Using the scale person you can also see that the wing area, when compared to even the Concorde, is quite small.
Yes, I agree that the wing seems to be too small and probably with an inefficient shape. I can't prove it, of course, especially as I don't know how large it actually is.
phavoc said:
Let's assume the image above has windows that aren't recessed (further increasing drag). What about the launch on top? That, too, will increase drag.
Yes, we don't know the drag either, do we?
Yet earlier you claimed, spcifically about the Subbie:
phavoc said:
... and (b) many designs have too much drag, such as the Type-R, that counter any lift, ...
I still don't understand what that means, given that drag and lift are perpendicular components of the same thing. How could it counter itself?
phavoc said:
The illustrations you have provided show craft with aerodynamic structure as well as wings designed specifically to create lift via airflow. I have continually acknowledged the fact that craft of this type (and weight) WILL generate lift as the descend. But that is possible only so long as they are moving forward at velocity (and no, I can't tell you their stall speed - though at 4,000 tons I would suspect it would be quite high).
The only illustration I used was of the Concorde. It can evidently take off, fly, and land on its own. Yet none of us can see that from the picture, can we? We can't even see the wing clearly. Which was my point.
phavoc said:
When you add all of this together what does it tell us? That these craft could descend from orbit, much like the shuttle could or the X-series lifting bodies did when dropped from an aircraft. But their design precludes them taking off like conventional aircraft using aerodynamic lift.
Yes, you have repeatedly stated that you believe that. Yet you can't back that up with a single measurement or even calculated lift example. That makes your statement just a guess as far as I can see.
And I will note again that even the lowly experimental TL6 X-24 (without any wings) could climb if it turned on some thrust. It is only without any thrust that it, and the shuttle, could only descend, just like any other aircraft. So I fail to see that it says just about anything about the Subbie with quite a lot of thrust.
phavoc said:
If you are asking for proof I would ask you the same. Unfortunately neither of us can provide proof for mythical craft.
Quite, I agree completely. Thank you for stating my point so eloquently.
So how can you state so categorically that no possible Traveller ship can fly?
phavoc said:
Traveller ships are (a) too heavy to generate lift for takeoff ...
phavoc said:
Therefore all we can do is provide current real-world examples of aircraft, physical and aerodynamic laws.
I agree completely that current aircraft can fly and that physics will continue to work in the future. But, as we seem to agree, we have very little reliable data about 'mythical craft'.
phavoc said:
And those laws, especially for flight, are very unforgiving when it comes to drag. And as anyone who's studied aerodynamics will tell you, drag is a bitch when you are trying to fly. Power can overcome a LOT of drag - but there is not only a limit, but also the more drag you have, the power you have to apply, and the more inefficient your flight profile becomes due to the fact that air compresses the faster you go, which increases both drag and the need for more power. And lift depends on air flowing faster underneath the wing than above it, hence the need for an angle of attack of the Type-R airfoil (or any Traveller craft thinking it can generate lift). If you look at the drawings for either the Concorde or An-225 you will see the wings are designed to do this.
Yes, that is a nice bit of waffle, and undoubtably correct, yet says nothing specific about any specific craft, much less all possible craft.
Laws of Physics are formulas, if you can't put numbers on the specific dependencies, you can't use them.
For a 4000 tonne Subbie in a 1 g gravity field we know that it weighs 4000 tonnes, aka it is pulled towards the planet by a force of 40 MN. Too see if it can take off we have to calculate if the lift (at the moment of take off with e.g. current air flow speed including wind, angle of attack, air density and viscosity) is bigger than, or smaller than, 40 MN. There is no way we can calculate actual lift for 'mythical craft', hence no way to determine if they can actually fly.
phavoc said:
Without all of this the ships cannot fly using real-world physics. To be specific, they cannot generate enough lift to stay aloft to land or takeoff using lift generated by aerodynamic effects. However, if you alter the equations by adding lift through some other means (such as thrusters or anti-gravity), then the formula would change. To determine that you have to provide all of the above requested information as well as the amount of lift being provided in another manner. For example, if the wings were able to provide 1% of the necessary lift to take off at say 100kts (you must have some airflow in order to generate lift), then the other 99% of the lifting force would need to come from some other mechanism (even from a repulsor grid if you had one).
Yes, I agree completely. But we still can't calculate lift for any specific 'mythical craft', much less all possible 'mythical craft', so we still don't know if they can fly.
phavoc said:
I don't suppose you'll agree with much of the above, but that's the basic science behind lift, and it's why I keep saying Traveller vessels can't utilize their structures to take off or land ...
Yes, I agree about the science but not about your extra assumptions. You just assume that lift is not sufficient, without demonstrating it. With specific numbers.
Without quantifying lift, which we can't do from an illustration, we don't know if any 'mythical craft' will fly. Without that we cannot, as you stated, 'provide proof for mythical craft'.
So I still don't understand how you so categorically can state that no possible Traveller ship can fly?
phavoc said:
Traveller ships are (a) too heavy to generate lift for takeoff ...