Solve ODE for variable domain

2020 9 3
1 个回答
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更新时间：2020 9 3
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Hi all
is it possible to solve the same ODE system for 3 adiacent different domain? Do i need something like that?
if x>x1&&x<=x2
.
.
.
elseif x>=x2&&x<x3
.
.
.
elseif x>x3
.
.
.
end
how continuity will be preserved?
Thank you for the help
Regards

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Alan Stevens
Alan Stevens 2020-9-3
What stops you solving it from x1 all the way past x3 in one go?
EldaEbrithil
EldaEbrithil 2020-9-3
because i am modeling a nozzle and the section of this nozzle varies along x so i need to cut the nozzle in 3 parts
Alan Stevens
Alan Stevens 2020-9-3
Doesn't that just mean you have something like area as a function of x? If you define it as a separate function, you could call it from within your ode section.
EldaEbrithil
EldaEbrithil 2020-9-3
function dYnozzledx=nozzlesinglebobb(x,Ynozzle,xstartconica,xfineconica,Ralfa_end,Rbeta_end,alfa_end_rad,beta_end_rad,xc_end,yc_end,Lnozzle_end,raggio_end,...
f1,f2,f3)
gamma=1.667;
Pt_nozzle=Ynozzle(1);
M_nozzle=Ynozzle(2);
if (x>=0)&&(x<xstartconica)
Anozzle= pi*((Rbeta_end*cos(beta_end_rad)-x)*tan(beta_end_rad))^2;
Perimetro=2*pi*((Rbeta_end*cos(beta_end_rad)-x)*tan(beta_end_rad));
%p=(Pt_nozzle/(1+((gamma-1)/2)*M_nozzle^2)^(gamma/(gamma-1)))
dA_nozzledx=(2*pi*tan(beta_end_rad)^2)*(x-Rbeta_end*cos(beta_end_rad));
dPt_nozzledx=-Pt_nozzle*(Perimetro*f1*gamma*M_nozzle^2)/(2*Anozzle*(Pt_nozzle/(1+((gamma-1)/2)*M_nozzle^2)^(gamma/(gamma-1)))*Anozzle);
dM_nozzledx=M_nozzle*((-(1+((gamma-1)/2)*M_nozzle^2)/(1-M_nozzle^2))*(dA_nozzledx/Anozzle)+...
((1+((gamma-1)/2)*M_nozzle^2)/(1-M_nozzle^2))*(gamma*(M_nozzle^2)*f1*Perimetro/(2*Anozzle*(Pt_nozzle/(1+((gamma-1)/2)*M_nozzle^2)^(gamma/(gamma-1)))*Anozzle)));
elseif (x>=xstartconica)&&(x<=xfineconica)
Anozzle= pi*(yc_end-sqrt(raggio_end^2-(x-xc_end)^2))^2;
Perimetro= 2*pi*(yc_end-sqrt(raggio_end^2-(x-xc_end)^2));
dA_nozzledx=(2*pi*(x-xc_end)/(sqrt(raggio_end^2-(x-xc_end)^2)))*(yc_end-sqrt(raggio_end^2-(x-xc_end)^2));
dPt_nozzledx=-Pt_nozzle*(Perimetro*f2*gamma*M_nozzle^2)/(2*Anozzle*(Pt_nozzle/(1+((gamma-1)/2)*M_nozzle^2)^(gamma/(gamma-1)))*Anozzle);
dM_nozzledx=M_nozzle*((-(1+((gamma-1)/2)*M_nozzle^2)/(1-M_nozzle^2))*(dA_nozzledx/Anozzle)+...
((1+((gamma-1)/2)*M_nozzle^2)/(1-M_nozzle^2))*(gamma*(M_nozzle^2)*f2*Perimetro/(2*Anozzle*(Pt_nozzle/(1+((gamma-1)/2)*M_nozzle^2)^(gamma/(gamma-1)))*Anozzle)));
elseif x>xfineconica
Anozzle= pi*((x-(Lnozzle_end-(Ralfa_end*cos(alfa_end_rad))))*tan(alfa_end_rad))^2;
Perimetro= 2*pi*((x-(Lnozzle_end-(Ralfa_end*cos(alfa_end_rad))))*tan(alfa_end_rad));
dA_nozzledx=(2*pi*tan(alfa_end_rad)^2)*(x-Lnozzle_end+Ralfa_end*cos(alfa_end_rad));
dPt_nozzledx=-Pt_nozzle*(Perimetro*f3*gamma*M_nozzle^2)/(2*Anozzle*(Pt_nozzle/(1+((gamma-1)/2)*M_nozzle^2)^(gamma/(gamma-1)))*Anozzle);
dM_nozzledx=M_nozzle*((-(1+((gamma-1)/2)*M_nozzle^2)/(1-M_nozzle^2))*(dA_nozzledx/Anozzle)+...
((1+((gamma-1)/2)*M_nozzle^2)/(1-M_nozzle^2))*(gamma*(M_nozzle^2)*f3*Perimetro/(2*Anozzle*(Pt_nozzle/(1+((gamma-1)/2)*M_nozzle^2)^(gamma/(gamma-1)))*Anozzle)));
end
dYnozzledx=[dPt_nozzledx;dM_nozzledx];
end
i need to subdived the domain because there are 3 different function that described the Section (Anozzle) trend
EldaEbrithil
EldaEbrithil 2020-9-3
as you can see the central part is a conical section

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 采纳的回答

Alan Stevens
Alan Stevens 2020-9-3

0 个投票

So you would then call your ode with something like:
[x,Y] = ode45(@nozzlesinglebobb, xspan, Y0,[],xstartconica,xfineconica,Ralfa_end,Rbeta_end,alfa_end_rad,beta_end_rad,xc_end,yc_end,Lnozzle_end,raggio_end,f1,f2,f3);
where xspan = [0 x_final] and Y0 = [Pt0; M0] or similar.
Then
Pt = Y(:,1);
M = Y(:,2);

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EldaEbrithil
EldaEbrithil 2020-9-3
编辑：EldaEbrithil 2020-9-3
I had written something that
[xSolnozzle,YSolnozzle]=ode23(@(x,Y)nozzlesinglebobb(x,Ynozzle,xstartconica,...
xfineconica,Ralfa_end,Rbeta_end,alfa_end_rad,beta_end_rad,xc_end,yc_end,Lnozzle_end,raggio_end,...
f1,f2,f3),xRangenozzle,Ynozzle);
is it correct?
Alan Stevens
Alan Stevens 2020-9-3
Does it work? If it does, great! If not, try the syntax I used

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