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Taylor Maccoll Eq. with Runge Kutta

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Old   November 21, 2015, 23:31
Default Taylor Maccoll Eq. with Runge Kutta
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yow
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Before I go use CFD, I wanted to approximate the supersonic flow field after a shock in front of a cone (0 deg. angle of attack). I used 4th order Runge Kutta with Taylor Maccoll eq. and am getting Vtheta = 0 at 31 deg cone half angle when I assume my shock beta = 34 deg. I've stared at my code for 20 h and have manually coded the Runge Kutta eq. as well as using ode45 function and get the same results. My step size is - .001. Can anyone please help? Maybe I'm just braindead...

Apologies if this is the wrong place to ask.
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Old   December 6, 2015, 12:22
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Nevermind, I found the answer after contemplating for a while... The initial Vtheta used for the Taylor-Maccoll equations must be negative to account for the decreasing Vr due to the flow relieving effect of the 3D cone surface.
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Old   April 29, 2021, 15:12
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I am having a similar issue. My RK4 is approximating a very high cone angle that is very close to the shock. What did you code your program in? I’m using Matlab. My initial conditions are right, though, so I don’t know what the issue is
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