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#1
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In terms of physics:
dive acceleration = earth gravitational constant + excess thrust / mass It is easy to see that as long as excess thrust is larger than zero, mass will reduce the planes acceleration. Excess thrust will be less than zero when the plane is above level speed for that power setting. Also, in typical flying conditions, earth gravitational constant >> excess thrust / mass, so excess thrust / mass doesn't really matter. If you don't care about physics, at least search for the TAIC test FC99 mentioned, read it, and adjust your expectations. That time would be a lot better spend than making another dozen posts on the issue here. |
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#2
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but I want to correct u in some point G actually the advantage to heavy planes see my formular posed previously. F= ma, a=(m*g - back force)/m when the backward force become larger and larger the mass * G will become more and more helpful to speed up the plane. that means the plane will bigger mass and less back force will be faster and the back force is complicate, it is regarded to the strenght of the plane, air wave darg force, pro pitch propeller tip speed, the shape of the wing, wing load and so on I dare not to simplify all this in to a univeral A = 8.7m/s as I calculated previously Do you still think I do not know physics? |
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#3
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to make it more obvious
set g=10, m = 10 , back force = 50 first plane mass = 2m second plane mass = 1m F=ma a1: a2 = (2m*g-backforce)/2m : (m*g-backforce)/m =150/20:50/10 =7.5:5 a1 is 50% faster |
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#4
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So in this extreme case plane have 2,5m/s advantage in acceleration. What will be the difference in distance after 12-13 seconds?
And in the end try with different values for drag for each plane like it is in most real life cases.
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Last edited by FC99; 04-27-2012 at 08:34 PM. |
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#5
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I just put everything simply in to the "backforce" even the air fricition and what so ever are supposed to be within the "back force" and if the missing drag u mentioned is the drag force by the engine JTD have already said Mass*G >> engine thrust or so "earth gravitational constant >> excess thrust / mass, so excess thrust / mass doesn't really matter." he is wrong? Last edited by mayshine; 04-27-2012 at 08:40 PM. |
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#6
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Just out of curiosity, how much difference you expect in dives?
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#7
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please do not be offenced, you know I just try to........ acutually i am happy to be wrong However I will try to provide more figures in the coming days so late here now |
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#8
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come on!!! in this extreme case it is not 2,5m/s advantage its 50 % speed acceleration advantage se FW = a1, La = a2 by the time la dive to from 300 to 500km/h , FW will get the speed of 600km/h enought to do a verticle hammer action. u know I can feel a lot of people are just defending theirself instead of looking for truth |
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#9
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Even with this numbers distance between the planes will be less than 200m. Now plug in real numbers for FW and La and do the calculation again. When you include real numbers for mass, drag and thrust difference between La and FW will be very small.
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#10
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LOL! You are so funny Mayshine. You tell us we aren't listening, and we don't know what we're talking about, but you have not listened to a bloody word anyone has said here, then you have the unmitigated gall to say that you would be happy to be proven wrong. That's Bull.
You are engaging in mental masturbation, pure and simple. Have fun.
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I'm pretty much just here for comic relief. Q6600@3.02 GHz, 4gig DDR2, GTX470, Win7 64bit |
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