x	Lbudget*qq
U	Us*vv
R	Rc0
Uw	0[m/s]
Vg	Vg0+A*x+4*pi*(R^3-Rc0^3)/3
Vdot	A*U+4*pi*R^2*Uw
pb	p0*(Vg0/Vg)^kap
pEl	0[Pa]
pRes	0[Pa]
Wgel	0[J]
Kgel	0[J]
Kjet	mJet*U^2/2
Esurf	pCap*A*x
ploss	Rloss*U+rho*Kloss*U*abs(U)/2
acc	outletOpen*(pb-pInf-pCap-ploss-rho*U^2/2)/(rho*L)
wallAcc	0[m/s^2]
Pdis	outletOpen*A*(Rloss*U^2+rho*Kloss*abs(U)^3/2)
Edis	E0*dd
Eout	E0*ee
Iout	Iscale*ii
Mout	rho*A*x
Pout	outletOpen*rho*A*U^3/2
energyResidual	(pb*Vg/(kap-1)-p0*Vg0/(kap-1)+pInf*(Vg-Vg0)+Kjet+Kgel+Wgel+Esurf+Edis+Eout)/E0
Fconf	pi*R^2*pEl
qJet	rho*U^2/2
Ijet	mJet*U
Fflux	rho*A*U^2
pArrestBound	Iout/(AObs*tObs)
stroke	x/Lbudget
stretch	R/Rc0
Mjet	abs(U)/cL
Mwall	abs(Uw)/cL
communication	L/cL*kap*abs(Vdot)/Vg