Thermal & Mechanical Properties of Matter Flashcards
Avogadro’s number
No of molecules in one mole
One mole contains 6.022x10^23 molecules
V^2
Vx^2+Vy^2+Vz^2
<Vx^2>=<Vy^2>=<Vz^2>
<V^2>= 3<Vx^2>
N
Number of molecules
n
Number of moles
Na
Avogadro’s number
Relating n, N and Na
N=n*Na
u
Mass of a mole of molecules =Nam
Number density
=u/V
Gas temperature
Measure of the random motion of molecules
Mean free time between collisions
Found by using inverse of Dan/dt
Mean free path
Multiply mean free time by velocity
Temperature of ideal gas
Measure of thermal kinetic energy of translation of molecules
Constant volume
All heat goes into Ek
Cv
3/2R
*perfect for monatomic, fails for diatomic/polyatomic
Heat flows into monatomic gas, constant volume
All goes to increase translational Ek
Diatomic
Additional Ek
Rotational and vibrational
Principle of equipartition of energy
Each component of energy has associated energy per molecule 1/2kbT
Degrees of freedom
Number of energy components to describe molecule completely
Dof monatomic
3 dof so 3/2kbT
Dof diatomic
5 dof so 5/2kbT
Dof vibrational
7 dof so 7/2kbT
For constant volume, dW
=0 so dQv=dKtr
For constant pressure dQp=
dKtr+dW
So dQp=dQv+dW
Cp=
Cv+R
Heat capacities of solids
Each atom: 3 Ek dof and 3 Ep dof so 6 dof
Average energy=6(1/2kbT) = 3kbT
f(v) allows what to be calculated
Most probable speed
Average speed
RMS speed
Most probable speed
df(v)/dv =0
Average speed
No of molecules having speeds in each interval
X by v, add up and divide by N
Integral between 0 and infinity of vf(v) dv
=root 8kbT/pi n
Mean square velocity
Integral between 0 and infinity of v^2f(v) dv
=3kbT/m
Root it for RMS
Pressure in fluids, if surface pressure increases
Pressure at all points increases by same amount
Archimedes principle
When a body is partially or completely immersed in a fluid, the fluid exerts an upward force on the body equal to the weight of the fluid displaced
Laminar flow
Steady
If cross sectional area reduced (laminar flow)
Becomes much faster
Eg if deep, wide river running slowly, faster when narrow and shallow
Bernoulli’s equation
p+pay+1/2pv^2= constant at all points
Applications of bernaoulli’s equation
Aeroplane wing
Stress
Measure of applied force causing deformation “force per unit area”
Strain
Measure of deformity
Elastic deformation
Returning to original shape once stress removed
Young’s modulus
Stress/strain
F/A / delta l/l
Units Nm^-2
Stiffness
Stress required to produce 100% strain
Bending
Both extension and compression
Bulk modulus
B= delta p / -delta v/ v0 still Nm^-2
Compressibility k
1/B
Graph of stress against strain for ductile material
y=x up to limit of proportionality
Gradient decreases until elastic limit
Then curves up and back down to fracture point
stress on y axis, strain on x
Stress strain graph for brittle material
y=x until limit of proportionality
Then gradient decreases for short length before fracture point