thermal properties of matter

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1
Temparature scales conversion equation
(reading on any scale -lower fixed point (ice point))/(upper fixed point(steam point)-lower fixed point) =constant i.e C/5=(F-32)/9=(K-273.15)/5
2
relation b/w Centigrade and fahrenheit and temperature change
C/5= F-32/9 ∆F=(9/5)∆C, ∆K=∆C
3
linear expansion,areal, volume formula
∆l=l*(alpha)*∆T, ∆A=A*(beta)*∆T, ∆V = V*(gamma)*∆T
4
relation b/w alpha,beta,gamma for isotropic material and their ratio
beta =2*alpha, gamma=3*alpha, ratio alpha:beta:gamma= 1:2:3
5
for same change in temperature if difference in length remains constant
L1*(alpha1)=L2*(aplha2)
6
equivalent temperature coefficient of linear expansion (in series,in parallel)
aplha(series)=(L1*aplha1+L2*aplha2)/L1+L2 , alpha(parallel)=(((aplha1)/L1)+(aplha2/L2))/((1/L1)+(1/L2))
7
effect of temperature on the time period of simple pendulum
T=2π√(l°(1+aplha*∆t) here ∆t is temperature difference l° is initial length,∆T/T=aplha*∆t/2 ,%timenlostor gain =(aplha*∆t/2) *100 , time lost or gain per day ∆T=43200*(alpha)*∆t
8
invar
invar =64%iron + 36% nickel (coefficient of linear expansion is very small for invar pendulum are made from invar to show correct time in all seasons)
9
error in scale reading due to expansion or contraction
TRUE VALUE=SR(1+aplha*∆T) ,SR: scale reading,here body do not expand ,due to linear expansion of scale the scale will expand and scale reading will be less than the true value at T' (if a scale gives correct reading at temperature T), however if T'<T due to contraction scale reading will be more than the true value ,so true value will still be given by the above equation ∆T=(T'-T) negative
10
thermal stress in rigidly fixed rod
strain =∆l/l°=alpha*∆T , young's modulus Y=Fl°/A*∆l
11
bi metallic strip
· Bimetallic strip works on the principle of differential expansion of metals
· If a bimetallic strip made of brass and iron is heated, brass bends on convex side (\alpha_{\text{brass}} > \alpha_{\text{Fe}})
· If it is cooled brass bends on concave side. The reason for this is expansion/ compression of brass is more than that of iron. Radius of curvature of bimetallic strip R=t/((alphabrass-alphaFe)∆T) where t is half the thickness of bimetallic strip used
12
expansion of cavity
Thermal expansion of an isotropic object may be imagined as a photographic enlargement. So if there is a hole A in a plate C (or cavity A inside a body C), the area of hole (or volume of cavity) will increase when body expands on heating, just as if the hole (or cavity) were solid B of the same material. Also the expansion of area (or volume) of the body C will be independent of shape and size of hole (or cavity), i.e., will be equal to that of D
13
EXPANSION OF LIQUID

(1) Liquid do not have linear and superficial expansion but these only have volume expansion
(2) Since liquids are always to be heated along with a vessel which contains them, so initially on heating the system (liquid + vessel), the level of liquid in vessel falls(as vessel expands more since it absorbs heat and liquid expands less) but later on, it starts rising due to faster expansion of the liquid

EXPANSION OF LIOUID
Expansion liquid is called real expansion.
Expansion of solid is called expansion of vessel
Observed expansion is called apparent expansion. gamma(real)=∆V(real)/V∆T. gamma(vessel)=∆Vvessel/V∆T. ∆Vapp=V∆T[gamma(real)-gamma(vessel)] also gamma(app)=gamma(real)-gamma(vessel)
14
gamma condition with ∆V and level of liquid
amma \Delta V Level
amma_{\text{real}} > amma_{\text{vessel}} (= 3\alpha) \Rightarrow amma_{\text{app}} > 0 \Delta V_{\text{app}} is positive Level of liquid in vessel will rise on heating
amma_{\text{real}} < amma_{\text{vessel}} (= 3\alpha) \Rightarrow amma_{\text{app}} < 0 \Delta V_{\text{app}} is negative Level of liquid in vessel will fall on heating
amma_{\text{real}} = amma_{\text{vessel}} (= 3\alpha) \Rightarrow amma_{\text{app}} = 0 \Delta V_{\text{app}} = 0 Level of liquid in vessel will remain same(look at DeepSeek)
15
variation of density with temperature
p'=p/(1+gamma*∆T) (for small temperature change p'=p(1-gamma*∆T)
16
ANOMALOUS EXPANSION OF WATER
Generally matter expands on heating and contracts on cooling. In case of water, it expands on heating if its temperature is greater than 4^{\circ}\text{C}. In the range 0^{\circ}\text{C} to 4^{\circ}\text{C}, water contracts on heating and expands on cooling. i.e amma is negative. This behaviour of water in the range from 0^{\circ}\text{C} to 4^{\circ}\text{C} is called anomalous expansion.
17
1 cal = how many joules
1 cal 4.2J
18
specific heat capacity (s) and what if s is dependent on temperature as s=f(T) the heat supplied to increase the then temperature from T1 to T2 is
s=∆Q/M∆T, ∆Q=integral from T1 to T2[M*s*dT]
19
heat capacity
s=∆Q/∆T
20
water equivalent of a body
∆Qwater=∆Qbody ,water equivalent=mass of body ×specific heat of the material
21
equilibrium temperature (when bodies at different temperatures are mixed without changing its state)
Teq=(m1s1T1+m2s2T2)/(m1s1+m2s2)
22
change of phase
solid to liquid (melting), liquid to solid (freezing), liquid to vapour(vaporisation),vapour to liquid (condensation) , solid to vapour (sublimation) Liquid to vapour (evaporation, without heating) melting happens at 0°C boiling happens at 100°C
23
EFFECT OF PRESSURE ON BOILING POINT
Boiling point increases with increase in pressure
If you close the steam outlet pressure increases ightarrow boiling stops. So more heat is required to boil again thus boiling point increases This is why pressure cooker cooks faster (BP of water > 100°C inside)
Similarly Boiling point decreases with decrease in pressure
24
TRIPLE POINT OF WATER
The specific temperature and pressure at which all three phases of water - Solid (Ice) liquid (water), and gas (Water vapor) - coexist simultaneously in thermodynamic equilibrium is called triple point.
25
latent heat
L=∆Q/m ,where m is in kg
26
latent heat of fusion for water (melting)
Lf=80cal or 3.36*10^5 Jkg^-1
27
latent heat of vaporization for water
Lv= 540 cal or 2.26*10^6 Jkg^-1
28
power (if constant)
power =∆Q/∆t , ms(ice)∆T/∆t1 =mLf/∆t2 =ms(water)∆T/∆t3. =mLv/∆t4
29
average rate of flow of heat
∆Q/∆t=KA(T1-T2)/l =-KA∆T/l where T1>T2 and ∆T = T2-T1 ,in differential form dQ/dt=-KAdT/dx, ∆Q/∆t Is called average heat current (H) H=-∆T/Rth (Rth=l/KA),unit of Rth is kelvin/Watt , dT/dx is called temperature gradient,heat flows in the direction of decreasing temperature
30
Temperature of intermediate junction
theta(i)=(theta1/R1+theta2/R2 +theta3/R3)/(1/R1+1/R2+1/R3) at study state rate of flow of heat through the conductor is constant
31
combination of conductor(series,parallel)
H is constant. Keq(series)=(L1+L2+l3)/((L1/k1)+(L2/k2)+(l3/k3)) , Keqparallel (length is same)K=(K1A1+K2A2+...+KnAn)/(A1+A2+...+An)
32
Emissive power(E)
E=Energy radiated/(area×time)
33
spectral emmisive power (E)
E=energy radiated/(Time*area*wavelength)=dQ/(dt*A*d(lamda) , total emissive power (E)=intergralfrim zero to infinity[E d(lamda)]
34
emissivity (e)
e=energy radiated by a body /energy radiated by ideal black body (ranges from 0<e<1 ,if e=0 no energy is radiated if e=1 then that body is perfect black body)
35
stefan's law(emissive power E) for black body and for normal body
E=sigmaT^4 ,where sigma is stefan's constant having dimension[MT^3theta^-4] and value is 5.67*10^-8 Wm^-2K^-4 for normal body E=e*sigma*T^4,Q=A*e*sigma*T^4*t , radiant power P=Q/t=A*e*sigma*T^4 P is proportional to R^2T^4,
36
stefan's law for body at temperature T surrounded by a body at T°
E=e*sigma(T^4-T°^4) ,for black body E=sigma(T^4-T°^4) note: good absorber is good emitter if the object is in thermal in equilibrium)
37
cooling by radiation
dT/dt= e*A*sigma(T^4-T°^4)/mc (where c is specific heat)
38
weins displacement law
lamda*T=b b is weins constant value is 2.89×10^-3 mK ,area under graph gives power of boder therefore A1/A2=[T1/T2]^4 ,height of peak is proportional to T^5
39
Newton's law of cooling
when T-T°>or =35°C, -dT/dt =K(T-T°)
40
temperature time equation
ln[Tf-T°]-ln[Ti-T°] or. ∆Tf=∆Ti e^-Kt
41
average temperature technique
T1-T2/t =K[(T1+T2)/2 -T°]
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