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![]() "Henri Wilson" HW@.... wrote in message ... On 16 Feb 2007 00:30:15 -0800, "George Dishman" wrote: On 16 Feb, 03:17, HW@....(Henri Wilson) wrote: On Thu, 15 Feb 2007 23:53:52 -0000, "George Dishman" wrote: "Henri Wilson" HW@.... wrote in message .. . On 15 Feb 2007 01:58:58 -0800, "George Dishman" wrote: .... There is a cyclic doppler shift. That means pulses come closer together then move apart again every orbit. If that isn't 'bunching' (of the pulses) what is? Ah, true. However that is a function of speed alone, I was talking of the bunching due to your variable speed which is in additional to the conventional effect. Here's the bit snipped from above: -:- Not quite, there is an interesting difference. The bunching effect depends on the acceleration and if you think of a circular orbit seen edge on, clearly the acceleration will vary 90 degrees out of phase with the velocity. For high speed and a short extinction distance the velocity will predominate while for low speed and long distance the acceleration will produce the larger contribution. George, you are refering to conventional doppler shift using constant c. This is not the same as bunching due to c+v changes. No, I'm describing ballistic theory, there is no acceleration term in conventional Doppler. -:- Yes...well I don't use equations anyway. I let the computer do the simulation...and there is no acceleration term .. although it might be present indirectly. Whatever, we both know qualitatively how the curves should look so we can check if your code gives a credible answer. Bottom line though is that previously I was not talking about conventional theory, please take more care as I understand very well what the consequences of your theory will be. The apparent maximum radial velocity using the conventional formula (invariant c) is 27983 m/s by my reckoning. I will get the same answer for the maximum....but it will occur at a slightly different phase. You should get the same as the conventional theory if you enter a distance of zero, a simple check to start. Then as you increase the distance the acceleration term will introduce a quadrature element which will change both the phase and amplitude. To keep the match to the amplitude, you can change the orbital inclination or the masses. The orbital inclination is already included in the radial velocity reading. Yes, as we said before, your velocity figure is actually v*sin(i). We both understand that. I have tried to explain this to Androcles but he cannot get it. There's lots he doesn't get but you and I understand it. No matter how an orbit is tilted, you can always rotate your telescope (and head) so that there exists an axis in the orbit plane that is perpendicular to your LOS. From that viewpoint, the radial velocities around the whole orbit are The 'edge on ones' simply multiplied by the same (unknown) cos factor. The measured radial velocities ARE those of the edge on orbit multiplied by cos(tilt)....so you cannot include it again. For circular orbits like this, that's true. For the purposes of predicting brightness curves, I only have to consider edge on orbits. My 'yaw angle' is that for an edge on orbit. It is not the conventional definition....but it works and it makes the programming much easier. For elliptical orbits in general you have to consider the angle between the major axis and the line of sight which I guess is your yaw, but for J1909-3744 we can ignore it. It doesn't matter what it is. If a circular orbit is tilted around an axis perpendicular to the LOS, the radial velocities around the whole orbit are multiplied by the same factor cos(tilt). That is already included in the observed velocity readings. Yes, what your program really tells you is v*sin(i) (using the standard convention for inclination) rather than v itself. It doesn't tell me anything about v. I FEED IN the measured value of maximum observed velocity (If I can get it). I don't think you quite understand the principle involved George. Trial and error Henry, you feed what you think is the true value of v*sin(i) and see whether the curves match the observations. If not you alter the value until you get a match and then you have found the value of v*sin(i). At that point the predicted velocity curve should match the published curve and you have found the true velocity which takes into account the effect of ballistic theory on the Doppler. Isn't that how you use it? However, consider the difference between a low speed orbit seen edge on and a high speed orbit at high inclination. Given that we know the period is 1.5 days, the high speed orbit requires either a higher mass companion or a smaller orbit. However, we know from spectroscopic analysis that the companion is a white dwarf with a surface temperature around 8500 degrees and a magnitude of about 21. That gives an indication of the mass so you can combine that with your result to work out limits for the inclination. Like I said, if you redefine YAW you don't have to worry about inclination. Yaw angle is the angle the major axis of an edge on orbit makes with the LOS. Ah, I guessed correctly :-) Anyway, put the numbers into your program and tell me what you get and then we can discuss their interpretation. Check the results for zero distance first and make sure you get the right speed and phase. Naturally for zero distance I get no brightness variation. The observed velocity is in phase with the true velocity. You should still get a very small variation due to the conventional bunching you reminded me of at the top. Then increase the distance to 3 light years but keep everything else the same and tell me how the amplitude and phase change. Those two checks should just confirm your software is working, after that we can try the more interesting questions of mass etc. and see if we can put some limits on the extinction distance. My software works. We'll see. It predicts brightness curves. Orbit inclination does not affect curve shape. I can predict the brightness curve of the dwarf companion. Where can I find the observed one? There is no observed brightness variation reported but that can probably only be taken to say any variation is less than 1 mag, the existing single measurements are no more accurate than that. I'm not sure what it is you are asking me to do. OK, let's do it in small steps so that I can give you clear questions. Common to all: set the eccentricity to zero, yaw becomes irrelevant. Set the orbital period to 1.5334494503 days. Step 1. Set the distance to zero (your sim should reproduce the conventional theory) and set the actual velocity to 27983 m/s. Check that the observed velocity curve you get matches that and that the maximum velocity is 90 degrees after conjunction. Step 2. Increase the distance until you just get the velocity curves going to infinity and tell me what distance you get. I am guessing that the critical distance should be around 4 light years but let's see what your program says before we get on to the more interesting stuff. George |
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