**Transfer function of Thermal System:**

#### Let us derive the formula for **transfer function of thermal system** and mathematical model of thermal System:

#### List of symbols used in **thermal system**.

#### q = Heat flow rate, Kcal/sec.

#### θ1 = Absolute temperature of emitter, °K.

#### θ2 = Absolute temperature of receiver, °K.

#### ∆θ = Temperature difference, °C.

#### A = Area normal to heat flow, m²

#### K = Conduction or Convection coefficient; Kcal/sec-°C.

#### Kr = Radiation coefficient, Kcal/sec-°C.

#### H = K/A=Convection coefficient, Kcal/m2-sec-°C.

#### H = Thermal conductivity , K cal/m-sec-°C.

#### ∆X = Thickness of conductor,m

#### R = Thermal resistance, °C-sec/Kcal

#### C = Thermal capacitance, Kcal/°C

####
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**Heat Flow Rate:**

**Thermal systems**are those that involve the transfer of heat from one substance to another.There are three difference ways of heat flow from one substance to another.They are conduction, convection and radiation.

For conduction,

Heat flow rate = q = K ∆θ = KA/∆X

For convection,

Heat flow rate, q= K ∆θ = HA ∆θ

#### For radiation,

#### Heat flow rate, q = Kr(θ1⁴ – θ2⁴)

#### If θ1 » θ2 then, q = Kr θ⁴

#### Where θ4 = (θ1⁴ – θ2⁴)¹/⁴

**Note :** θ4 is called effective temperature difference of the emitter and receiver.

**Mathematical model of thermal system: **

#### The **model of thermal systems** are obtained by using thermal resistance and capacitance which are the basic elements of the **thermal system**.The thermal resistance and capacitance are distributed in nature.But for simplicity in analysis lumped parameter models are used.

#### In lumped parameter model it is assumed that the substances that are characterized by resistance to heat flow have negligible heat capacitance and the substances that are characterized by heat capacitance have negligible resistance to heat flow.The thermal resistance, R for heat transfer between two substances is defined as the ratio of change in temperature and change in heat flow rate.

#### The thermal resistance, R for heat transfer between two substances is defined as the ratio of change in temperature and change in heat flow rate.

####
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#### For conduction or convection,

#### Heat flow rate, q = K ∆θ

#### On differentiating we get,

#### dq = K d(∆θ)

#### d(∆θ)/dq = 1/K

#### But thermal resistance, R = d(∆θ)/dq

#### Thermal resistance, R = 1/K for conduction

#### = 1/K = 1/HA = for convection

#### For radiation,

Heat flow rate, q = Krθ⁴

On differentiating we get

dq = Kr 4 θ³ dθ

dθ/dq = 1/Kr4 θ³

But thermal resistance, R = dθ/dq

Thermal resistance, R = 1/4Kr θ³ (for radiation)

#### Thermal Capacitance, C is defined as the ratio of change in heat stored and change in temperature.

#### Let M = Mass of substance considered, Kg

#### c = Specific heat of substance, Kcal/Kg -°C

#### Now, Thermal capacitance, C = Mcp

####
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**Transfer function of Thermal system: **

#### Consider a simple **thermal system** shown in the below figure.Let us assume that the tank is insulated to eliminate heat loss to the surrounding air, there is no heat storage in the insulation and liquid in the tank is kept at uniform temperature by perfect mixing with the help of a stirrer.Thus, a single temperature is used to describe the temperature of the liquid in the tank and of the out flowing liquid.The **transfer function of thermal system** can be derived as shown below.

#### Let θ1 = Steady state temperature of inflowing liquid, °C

#### θ0 = Sandy state temperature of outflowing liquid, °C

#### G = Steady state liquid flow rate, Kg/sec

#### M = Mass of liquid in tank, Kg

#### c = Specific heat of liquid, Kcal/Kg °C

#### R = Thermal resistance, °C – sec/Kcal

#### C = Thermal capacitance, Kcal/°C

#### Q = Steady state heat input rate, Kcal/Sec

#### Let us assume that the temperature of inflowing liquid is kept constant. Let the heat input rate to the **thermal system** supplied by the heater is suddenly changed from Q to Q + q1.Due to this, the heat output flow rate will gradually change from Q to Q + q0.The temperature of the outflowing liquid will also be changed from θ0 to θ0 + θ.

####
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#### For this system the equation for q0, C and R are obtained as follows,

#### Thermal capacitance, C = Mass, M x Specific heat of liquid, c = Mc

#### On substituting for qo from equation (1) in equation (3) we get,

#### In this **thermal system**,rate of change of temperature is directly proportional to change in heat input rate.

The constant of proportionality is capacitance C of the system.