The non-linear dynamic behavior of a nonisothermal CSTR is linearized by expanding its nonlinear balance equations around a steady-state operating point and retaining only first-order terms. The main nonlinearity comes from the Arrhenius reaction rate, (k(T)c_A = k_0 e^{-E/(RT)}c_A), because temperature affects the reaction rate exponentially while concentration affects it directly. The resulting deviation-variable model is a coupled set of linear differential equations suitable for stability, transient-response, and control analysis.
A nonisothermal CSTR is linearized locally, not globally: the nonlinear mass and energy balances are replaced by their first-order Taylor approximation around a selected steady state. This produces a linear state-space model that accurately describes small deviations in concentration, temperature, flow, feed conditions, and cooling duty.
Why the CSTR Model Is Nonlinear
The Component Balance
For a first-order reaction, the reactant balance can be written as
[ \frac{dc_A}{dt}
\frac{F_i}{V}(c_{Ai}-c_A)
k_0e^{-E/(RT)}c_A ]
The nonlinear term is the reaction rate,
[ r_A=k_0e^{-E/(RT)}c_A ]
The exponential temperature dependence is the dominant source of nonlinearity.
The Energy Balance
The reactor energy balance is
[ \frac{dT}{dt}
\frac{F_i}{V}(T_i-T) + \frac{(-\Delta H_r)k_0e^{-E/(RT)}c_A}{\rho c_p}
\frac{Q}{\rho c_pV} ]
For an exothermic reaction, an increase in temperature increases the reaction rate, which generates additional heat. That heat can further increase the temperature, creating the feedback responsible for thermal sensitivity, multiple steady states, and potential instability.
The Volume Balance
The total mass balance is
[ \frac{dV}{dt}=F_i-F ]
If inlet and outlet flows are maintained equally, the reactor volume is approximately constant and the principal dynamic states are concentration and temperature. If level or flow dynamics are important, (V) is retained as an additional state during linearization.
Selecting the Operating Point
Steady-State Conditions
Choose a nominal steady state defined by
[ \bar{c}_A,\quad \bar{T},\quad \bar{V},\quad \bar{F}i,\quad \bar{c}{Ai},\quad \bar{T}_i,\quad \bar{Q} ]
At steady state, the derivatives of the state variables are zero:
[ \left.\frac{dc_A}{dt}\right|{\mathrm{ss}}=0, \qquad \left.\frac{dT}{dt}\right|{\mathrm{ss}}=0, \qquad \left.\frac{dV}{dt}\right|_{\mathrm{ss}}=0 ]
The steady-state balances establish the reference point about which the model is approximated.
Deviation Variables
Each process variable is expressed as its steady-state value plus a small deviation:
[ c_A=\bar{c}_A+\Delta c_A ]
[ T=\bar{T}+\Delta T ]
[ V=\bar{V}+\Delta V ]
Inputs and disturbances are treated similarly:
[ Q=\bar{Q}+\Delta Q, \qquad c_{Ai}=\bar{c}{Ai}+\Delta c{Ai}, \qquad T_i=\bar{T}_i+\Delta T_i ]
The deviation variables describe how far the plant has moved from its nominal operating condition.
Linearizing the Arrhenius Reaction Rate
First-Order Taylor Expansion
Define the nonlinear reaction-rate function as
[ r(c_A,T)=k_0e^{-E/(RT)}c_A ]
A two-variable Taylor expansion around ((\bar{c}_A,\bar{T})) gives
[ r(c_A,T) \approx r(\bar{c}A,\bar{T}) + \left.\frac{\partial r}{\partial c_A}\right|{\mathrm{ss}}\Delta c_A + \left.\frac{\partial r}{\partial T}\right|_{\mathrm{ss}}\Delta T ]
Terms involving products such as (\Delta c_A\Delta T), as well as second- and higher-order terms, are neglected.
Evaluating the Derivatives
The nominal rate constant is
[ \bar{k}=k_0e^{-E/(R\bar{T})} ]
Therefore,
[ \left.\frac{\partial r}{\partial c_A}\right|_{\mathrm{ss}}
\bar{k} ]
and
[ \left.\frac{\partial r}{\partial T}\right|_{\mathrm{ss}}
\bar{k}\bar{c}_A \frac{E}{R\bar{T}^{2}} ]
The linearized reaction rate becomes
[ \Delta r \approx \bar{k}\Delta c_A + \bar{k}\bar{c}_A \frac{E}{R\bar{T}^{2}}\Delta T ]
or, equivalently,
[ r \approx \bar{r} + \bar{k}\Delta c_A + \bar{k}\bar{c}_A \frac{E}{R\bar{T}^{2}}\Delta T ]
This expression shows directly how concentration and temperature perturbations alter the reaction rate near the chosen operating point.
Forming the Linearized Dynamic Model
Fixed-Volume Approximation
For a constant-volume reactor with (F_i=F=\bar{F}), the concentration balance becomes
[ \frac{dc_A}{dt}
\frac{\bar{F}}{\bar{V}}(c_{Ai}-c_A)
r(c_A,T) ]
After substituting the Taylor approximation and cancelling the steady-state terms,
[ \frac{d\Delta c_A}{dt}
\left( \frac{\bar{F}}{\bar{V}}+\bar{k} \right)\Delta c_A
\bar{k}\bar{c}A \frac{E}{R\bar{T}^{2}}\Delta T + \frac{\bar{F}}{\bar{V}}\Delta c{Ai} ]
This equation describes the local concentration dynamics as a linear combination of concentration, temperature, and feed-concentration deviations.
Linearized Energy Balance
Define
[ \alpha=\frac{-\Delta H_r}{\rho c_p} ]
The reaction-heat contribution is (\alpha r). The linearized energy balance is then
[ \frac{d\Delta T}{dt}
\alpha\bar{k}\Delta c_A + \left[ -\frac{\bar{F}}{\bar{V}} + \alpha\bar{k}\bar{c}_A \frac{E}{R\bar{T}^{2}} \right]\Delta T + \frac{\bar{F}}{\bar{V}}\Delta T_i
\frac{1}{\rho c_p\bar{V}}\Delta Q ]
The temperature equation contains the local thermal feedback. The coefficient multiplying (\Delta T) reflects the competition between convective cooling and the increase in heat generation caused by a temperature rise.
Including Volume or Flow Dynamics
If the reactor volume is not constant, the volume balance is also linearized:
[ \frac{d\Delta V}{dt}=\Delta F_i-\Delta F ]
The factors (F_i/V) in the concentration and energy balances must then be expanded as well. For example, the first-order approximation of the inlet dilution term is
[ \frac{F_i}{V} \approx \frac{\bar{F}_i}{\bar{V}} + \frac{1}{\bar{V}}\Delta F_i
\frac{\bar{F}_i}{\bar{V}^{2}}\Delta V ]
This introduces coupling between flow, liquid volume, concentration, and temperature.
Expressing the Model in State-Space Form
State, Input, and Disturbance Vectors
A typical state vector is
[ x= \begin{bmatrix} c_A\ T\ V \end{bmatrix} ]
For a constant-volume analysis, it may be reduced to
[ x= \begin{bmatrix} c_A\ T \end{bmatrix} ]
Manipulated variables can include cooling duty (Q), outlet flow (F), or coolant flow through a jacket. Feed concentration, feed temperature, and inlet flow are commonly treated as disturbances.
Jacobian Representation
The nonlinear model can be written generally as
[ \dot{x}=f(x,u,d) ]
where (x) contains the states, (u) the manipulated inputs, and (d) the disturbances. Linearizing around the steady state gives
[ \Delta\dot{x}
A\Delta x+B\Delta u+E\Delta d ]
with
[ A= \left.\frac{\partial f}{\partial x}\right|{\mathrm{ss}}, \qquad B= \left.\frac{\partial f}{\partial u}\right|{\mathrm{ss}}, \qquad E= \left.\frac{\partial f}{\partial d}\right|_{\mathrm{ss}} ]
The output equation is similarly written as
[ \Delta y=C\Delta x+D\Delta u ]
This state-space form is the standard basis for process-control analysis.
What the Linear Model Reveals
Local Stability
The eigenvalues of the state matrix (A) determine local stability. If all eigenvalues have negative real parts, small perturbations decay and the selected steady state is locally stable.
If at least one eigenvalue has a positive real part, small deviations grow and the steady state is locally unstable.
Transient Response
The linear model predicts how concentration and temperature respond to small changes in cooling duty, feed concentration, feed temperature, or flow rate. It can be used to estimate response speed, overshoot, interaction between variables, and dominant time constants.
Heat-Transfer Control
The cooling duty (Q) appears as an input to the energy balance. This makes the linearized model useful for evaluating temperature-control strategies, including feedback or cascade control involving reactor temperature and jacket or coolant flow.
Multiple Operating Points
A nonisothermal CSTR can have more than one steady state because reaction heat generation increases strongly with temperature while heat removal responds through flow and cooling mechanisms. Each steady state has its own Jacobian and therefore its own local dynamic behavior.
A linear model developed around one operating point should not automatically be used to represent the dynamics near another operating point.
Understanding the Trade-offs
The Model Is Only Locally Accurate
The Taylor approximation is reliable for sufficiently small deviations from the selected steady state. Large temperature or concentration changes can make the neglected higher-order terms significant.
For startup, shutdown, large disturbances, or transitions between steady states, the original nonlinear model should be simulated.
Strong Thermal Sensitivity Can Limit Accuracy
Because the Arrhenius term changes exponentially with temperature, even moderate temperature deviations may produce substantial rate changes. A linear model may therefore lose accuracy sooner in a highly exothermic or high-activation-energy system than in a weakly temperature-sensitive system.
Constant-Volume Assumptions May Hide Important Dynamics
Assuming (F_i=F) simplifies the model by removing volume dynamics. That assumption is inappropriate when level changes, unequal inlet and outlet flows, or flow-control dynamics materially affect the reactor response.
Linearization Does Not Determine Global Stability
Eigenvalue analysis describes behavior near one operating point. It cannot by itself establish the behavior of the full nonlinear reactor across all possible temperatures, concentrations, or flow conditions.
How to Apply This to Your Project
The appropriate linearization procedure depends on the analysis objective and the variables that are actively controlled.
- If your primary focus is local stability: Solve the steady-state balances, compute the Jacobian matrix at that operating point, and inspect the eigenvalues of (A).
- If your primary focus is temperature control: Retain the Arrhenius temperature derivative and use cooling duty or coolant flow as the manipulated input.
- If your primary focus is composition control: Include concentration as a controlled output and analyze the effects of feed concentration, feed flow, and temperature disturbances.
- If your primary focus is level or flow control: Retain the volume balance and linearize the (F_i/V) terms instead of assuming constant volume.
- If your primary focus is large transients or runaway behavior: Use the full nonlinear mass and energy balances, because a single local linear model cannot capture global thermal behavior.
The essential process-control model is obtained by evaluating the first derivatives of the nonlinear CSTR balances at a steady state, converting the reactor into a local linear system for rigorous small-signal analysis.
Summary Table:
| Key Aspect | Summary |
|---|---|
| Main nonlinearity | Arrhenius reaction kinetics, where temperature affects reaction rate exponentially. |
| Operating point | A selected steady state defined by nominal concentration, temperature, volume, flow, feed, and cooling conditions. |
| Linearization method | First-order Taylor expansion of the nonlinear mass and energy balances. |
| Main states | Reactant concentration and temperature; reactor volume is included when level or flow dynamics matter. |
| Linear model | Deviation-variable form: Δẋ = AΔx + BΔu + EΔd. |
| Control inputs | Cooling duty, coolant flow, outlet flow, or other manipulated variables. |
| Analysis applications | Local stability, transient response, time constants, process interactions, and temperature-control design. |
| Key limitation | The model is locally accurate and should not replace the nonlinear model for large transients or runaway analysis. |
Planning a CSTR pilot plant for teaching, research, process development, or industrial validation? Contact LABPARK to discuss your requirements. LABPARK provides Educational and Vocational Unit Operations Pilot Plants for chemical engineering, bioprocess and biotech, and environmental and water treatment applications. Our team can help universities, research institutes, and enterprises select an appropriate nonisothermal CSTR system, configure measurement and control functions, and match the pilot plant to studies involving reaction kinetics, heat transfer, process control, stability, and scale-up. Contact us to develop a practical, reliable pilot-plant solution that supports hands-on training, repeatable experiments, and advanced process-control research.
Related Products
- Multi-Stage Stirred Tanks in Series Residence Time Distribution and Mixing Performance Determination Educational Pilot Plant
- Residence Time Distribution and Reactor Flow Characteristics Determination Educational Pilot Plant
- Multi Functional Catalytic Reaction and Reactor Evaluation Educational Unit Operations Pilot Plant
- Gas Phase Mixing and Residence Time Distribution Determination Educational Unit Operations Pilot Plant
- Multi-Reactor Educational Pilot Plant for Reaction Engineering Unit Operations
People Also Ask
- CSTR Multiplicity: Which physical variables map to universal unfolding?
- How does impeller configuration affect RTD & reactor performance? Optimize mixing and conversion in pilot plants.
- How do multiple CSTRs in series affect stability? Master Complex Pilot Plant Dynamics
- How does MRF model impeller rotation in CFD? Key Boundary Conditions Explained
- How can a CSTR pilot plant demonstrate reactor staging? Visualize volume savings.