Current Affairs JEE Main & Advanced

(1) To rectify the errors caused by ignoring the intermolecular forces of attraction and the volume occupied by molecules, Vander Waal (in 1873) modified the ideal gas equation by introducing two corrections,   (i) Volume correction              (ii)  Pressure correction   (2) Vander Waal's equation is obeyed by the real gases over wide range of temperatures and pressures, hence it is called equation of state for the real gases.   (3) The Vander Waal's equation for n moles of the gas is,     \[\underset{\begin{smallmatrix} \text{Pressure correction} \\ \text{for molecular attraction} \end{smallmatrix}}{\mathop{\left( P+\frac{{{n}^{2}}a}{{{V}^{2}}} \right)}}\,\underset{\begin{smallmatrix} \\  \text{Volume correction for } \\ \text{finite size of molecules} \end{smallmatrix}}{\mathop{[V-nb]}}\,=nRT\]   a and b are Vander Waal's constants whose values depend on the nature of the gas. Normally for a gas \[a>>b\].   (i) Constant a : It is a indirect measure of magnitude of attractive forces between the molecules. Greater is the value of a, more easily the gas can be liquefied. Thus the easily liquefiable gases (like \[S{{O}_{2}}>N{{H}_{3}}>{{H}_{2}}S>C{{O}_{2}})\] have high values than the permanent gases (like \[{{N}_{2}}>{{O}_{2}}>{{H}_{2}}>He)\].   Units of 'a' are : atm.\[{{L}^{2}}\,mo{{l}^{-2}}\] or atm.\[{{m}^{6}}mo{{l}^{-2}}\] or \[N\,{{m}^{4}}\,mo{{l}^{-2}}\](S.I. unit).   (ii) Constant b : Also called co-volume or excluded volume,   \[b=4{{N}_{0}}v=4{{N}_{0}}\left( \frac{4}{3}\pi {{r}^{3}} \right)\]   It's value gives an idea about the effective size of gas molecules. Greater is the value of b, larger is the size and smaller is the compressible volume. As b is the effective volume of the gas molecules, the constant value of b for any gas over a wide range of temperature and pressure indicates that the gas molecules are incompressible.   Units of 'b' are : \[L\,mo{{l}^{-1}}\] or \[{{m}^{3}}\,mo{{l}^{-1}}\](S.I. unit)   (iii) The two Vander Waal's constants and Boyle's temperature \[({{T}_{B}})\] are related as,   \[{{T}_{B}}=\frac{a}{bR}\]   (4) Vander Waal's equation at different temperature and pressures   (i) When pressure is extremely low : For one mole of gas,   \[\left( P+\frac{a}{{{V}^{2}}} \right)\,(V-b)=RT\] or \[PV=RT-\frac{a}{V}+Pb+\frac{ab}{{{V}^{2}}}\]   (ii) When pressure is extremely high : For one mole of gas,   \[PV=RT+Pb\]; \[\frac{PV}{RT}=1+\frac{Pb}{RT}\]  or \[Z=1+\frac{Pb}{RT}\]   where Z is compressibility factor.   (iii) When temperature is extremely high : For one mole of gas,   \[PV=RT\].   (iv) When pressure is low : For one mole of gas,   \[\left( P+\frac{a}{{{V}^{2}}} \right)\,(V-b)=RT\] or \[PV=RT+Pb-\frac{a}{V}+\frac{ab}{{{V}^{2}}}\]   or \[\frac{PV}{RT}=1-\frac{a}{VRT}\] or \[Z=1-\frac{a}{VRT}\]   (v) For hydrogen : Molecular mass of hydrogen is small hence value of 'a' will be small owing to smaller intermolecular force. Thus the terms \[\frac{a}{V}\] and \[\frac{ab}{{{V}^{2}}}\] may be ignored. Then Vander Waal's equation becomes,   \[PV=RT+Pb\]  or \[\frac{PV}{RT}=1+\frac{Pb}{RT}\]   or \[Z=1+\frac{Pb}{RT}\]   In case of hydrogen, compressibility factor is always greater than one.   (5) Merits of Vander Waal's equation   (i) The Vander Waal's equation holds good for real gases upto moderately high pressures.   (ii) The equation represents the trend of the isotherms representing the variation of PV with P for various gases.   (iii) From the Vander Waal's equation it is possible to obtain expressions of Boyle's temperature, critical constants and inversion temperature in terms of the Vander Waal's constants more...

(1) Gases which obey gas laws or ideal gas equation \[(PV=nRT)\] at all temperatures and pressures are called ideal or perfect gases. Almost all gases deviate from the ideal behaviour i.e., no gas is perfect and the concept of perfect gas is only theoretical.   (2) Gases tend to show ideal behaviour more and more as the temperature rises above the boiling point of their liquefied forms and the pressure is lowered. Such gases are known as real or non ideal gases. Thus, a “real gas is that which obeys the gas laws under low pressure or high  temperature”.   (3) The deviations can be displayed, by plotting the P-V isotherms of real gas and ideal gas.     (4) It is difficult to determine quantitatively the deviation of a real gas from ideal gas behaviour from the P-V isotherm curve as shown above. Compressibility factor Z defined by the equation,   \[PV=ZnRT\] or \[Z=PV/nRT=P{{V}_{m}}/RT\]   is more suitable for a quantitative description of the deviation from ideal gas behaviour.   (5) Greater is the departure of Z from unity, more is the deviation from ideal behaviour. Thus, when   (i) \[Z=1\], the gas is ideal at all temperatures and pressures. In case of \[{{N}_{2}}\], the value of Z is close to 1 at \[{{50}^{o}}C\]. This temperature at which a real gas exhibits ideal behaviour, for considerable range of pressure, is known as Boyle's temperature or Boyle's point \[({{T}_{B}})\].   (ii) \[Z>1\], the gas is less compressible than expected from ideal behaviour and shows positive deviation, usual at high P i.e. \[PV>RT\].   (iii) \[Z<1\], the gas is more compressible than expected from ideal behaviour and shows negative deviation, usually at low P i.e. \[PV<RT\].   (iv) \[Z>1\] for \[{{H}_{2}}\] and He at all pressure i.e., always shows positive deviation.   (v) The most easily liquefiable and highly soluble gases \[(N{{H}_{3}},\,S{{O}_{2}})\] show larger deviations from ideal behaviour i.e. \[Z<<1\].   (vi) Some gases like \[C{{O}_{2}}\] show both negative and positive deviation.   (6) Causes of deviations of real gases from ideal behaviour : The ideal gas laws can be derived from the kinetic theory of gases which is based on the following two important assumptions,   (i) The volume occupied by the molecules is negligible in comparison to the total volume of gas.   (ii) The molecules exert no forces of attraction upon one another. It is because neither of these assumptions can be regarded as applicable to real gases that the latter show departure from the ideal behaviour.  

(1) At any particular time, in the given sample of gas all the molecules do not possess same speed, due to the frequent molecular collisions with the walls of the container and also with one another, the molecules move with ever changing speeds and also with ever changing direction of motion.   (2) According to Maxwell, at a particular temperature the distribution of speeds remains constant and this distribution is referred to as the Maxwell-Boltzmann distribution  and given by the following expression,   \[\frac{d{{n}_{0}}}{n}=4\pi {{\left( \frac{M}{2\pi RT} \right)}^{3/2}}.{{e}^{-M{{u}^{2}}/2RT}}.{{u}^{2}}dc\]   where, \[d{{n}_{0}}=\] Number of molecules out of total number of molecules n, having velocities between c and \[c+dc\], \[d{{n}_{0}}/n=\]Fraction of the total number of molecules, M = molecular weight, T = absolute temperature. The exponential factor \[{{e}^{-M{{u}^{2}}/2RT}}\] is called Boltzmann factor.   (3) Maxwell gave distribution curves of molecular speeds for \[C{{O}_{2}}\] at different temperatures. Special features of the curve are :   (i) Fraction of molecules with two high or two low speeds is very small.   (ii) No molecules has zero velocity.   (iii) Initially the fraction of molecules increases in velocity till the peak of the curve which pertains to most probable velocity and thereafter it falls with increase in velocity.     (4) Types of molecular speeds or Velocities   (i) Root mean square velocity \[({{u}_{rms}})\] : It is the square root of the mean of the squares of the velocity of a large number of molecules of the same gas.   \[{{u}_{rms}}=\sqrt{\frac{u_{1}^{2}+u_{2}^{2}+u_{3}^{2}+.....u_{n}^{2}}{n}}\]   \[{{u}_{rms}}=\sqrt{\frac{3PV}{(m{{N}_{0}})=M}}=\sqrt{\frac{3RT}{(m{{N}_{0}})=M}}\]\[=\sqrt{\frac{3RT}{M}}=\sqrt{\frac{3kT}{m}}=\sqrt{\frac{3P}{d}}\]   where k = Boltzmann constant \[=\frac{R}{{{N}_{0}}}\]   (a)  For the same gas at two different temperatures, the ratio of RMS velocities will be, \[\frac{{{u}_{1}}}{{{u}_{2}}}=\sqrt{\frac{{{T}_{1}}}{{{T}_{2}}}}\]   (b) For two different gases at the same temperature, the ratio of RMS velocities will be, \[\frac{{{u}_{1}}}{{{u}_{2}}}=\sqrt{\frac{{{M}_{2}}}{{{M}_{1}}}}\]   (c) RMS velocity at any temperature \[{{t}^{o}}C\] may be related to its value at S.T.P. as, \[{{u}_{t}}=\sqrt{\frac{3P(273+t)}{273d}}\].   (ii) Average velocity \[({{v}_{av}})\] : It is the average of the various velocities possessed by the molecules.   \[{{v}_{av}}=\frac{{{v}_{1}}+{{v}_{2}}+{{v}_{3}}+......{{v}_{n}}}{n}\];  \[{{v}_{av}}=\sqrt{\frac{8RT}{\pi M}}=\sqrt{\frac{8kT}{\pi m}}\]   (iii) Most probable velocity \[({{\alpha }_{mp}})\]: It is the velocity possessed by maximum number of molecules of a gas at a given temperature.   \[{{\alpha }_{mp}}=\sqrt{\frac{2RT}{M}}=\sqrt{\frac{2PV}{M}}=\sqrt{\frac{2P}{d}}\]   (5) Relation between molecular speeds or velocities,   (i) Relation between \[{{u}_{rms}}\] and \[{{v}_{av}}\]: \[{{v}_{av}}=0.9213\times {{u}_{rms}}\]  or \[{{u}_{rms}}=1.085\times {{v}_{av}}\]   (ii) Relation between \[{{\alpha }_{mp}}\] and \[{{u}_{rms}}\]: \[{{\alpha }_{mp}}=0.816\times {{u}_{rms}}\]  or \[{{u}_{rms}}=1.224\times {{\alpha }_{mp}}\]   (iii) Relation between \[{{\alpha }_{mp}}\] and \[{{v}_{av}}\]: \[{{v}_{av}}=1.128\times {{\alpha }_{mp}}\]   (iv) Relation between \[{{\alpha }_{mp}}\], \[{{v}_{av}}\] and \[{{u}_{rms}}\]   \[{{\alpha }_{mp}}\]            :    \[{{v}_{av}}\]       :         \[{{u}_{rms}}\]   \[\sqrt{\frac{2RT}{M}}\]      :    \[\sqrt{\frac{8RT}{\pi M}}\]   :        \[\sqrt{\frac{3RT}{M}}\]   \[\sqrt{2}\]              :   \[\sqrt{\frac{8}{\pi }}\]          :          \[\sqrt{3}\]   1.414      :    1.595     :           1.732   1              :    1.128     :           1.224    i.e., \[{{\alpha }_{mp}}<{{v}_{av}}<{{u}_{rms}}\]  

(1) The closest distance between the centres of two molecules taking part in a collision is called molecular or collision diameter \[(\sigma )\]. The molecular diameter of all the gases is nearly same lying in the order of \[{{10}^{-8}}\,cm\].     (2) The number of collisions taking place in unit time per unit volume, called collision frequency (z).   (i) The number of collision made by a single molecule with other molecules per unit time are given by, \[{{Z}_{A}}=\sqrt{2}\pi {{\sigma }^{2}}{{u}_{\text{av}\text{.}}}n\] where n is the number of molecules per unit molar volume, \[n=\frac{\text{Avogadro number(}{{N}_{0}}\text{)}}{{{V}_{m}}}=\frac{6.02\times {{10}^{23}}}{0.0224}{{m}^{-3}}\]   (ii) The total number of bimolecular collision per unit time are given by, \[{{Z}_{AA}}=\frac{1}{\sqrt{2}}\pi {{\sigma }^{2}}{{u}_{\text{av}.}}{{n}^{2}}\]   (iii) If the collisions involve two unlike molecules, the number of bimolecular collision are given by, \[{{Z}_{AB}}=\sigma _{AB}^{2}{{\left[ 8\pi RT\frac{({{M}_{A}}+{{M}_{B}})}{{{M}_{A}}{{M}_{B}}} \right]}^{1/2}}\]where, \[{{\sigma }_{AB}}=\frac{{{\sigma }_{A}}+{{\sigma }_{B}}}{2}\]   \[{{M}_{A}}\], \[{{M}_{B}}\] are molecular weights \[(M=m{{N}_{0}})\]   (iv) (a) At particular temperature; \[Z\propto {{p}^{2}}\]   (b) At particular pressure; \[Z\propto {{T}^{-3/2}}\]   (c) At particular volume; \[Z\propto {{T}^{1/2}}\]   (3) During molecular collisions a molecule covers a small distance before it gets deflected. The average distance travelled by the gas molecules between two successive collision is called mean free path \[(\lambda )\].   \[\lambda =\frac{\text{Average distance travelled per unit time(}{{u}_{\text{av}}}\text{)}}{\text{No}\text{. of collisions made by single molecule per unit time (}{{Z}_{A}}\text{)}}\]   \[=\frac{{{u}_{\text{av}}}}{\sqrt{\text{2}}\pi {{\sigma }^{2}}{{u}_{\text{avr}\text{.}}}n}=\frac{1}{\sqrt{2}\pi n{{\sigma }^{2}}}\]   (i) Larger the size of the molecules, smaller the mean free path, i.e., \[\lambda \propto \frac{1}{{{\text{(radius)}}^{\text{2}}}}\]   (ii)  Greater the number of molecules per unit volume, smaller the mean free path.   (iii) Larger the temperature, larger the mean free path.   (iv) Larger the pressure, smaller the mean free path.   (5) Relation between collision frequency (Z) and mean free path (l) is given by,  \[Z=\frac{{{u}_{rms}}}{\lambda }\]  

(1) Kinetic theory was developed by Bernoulli, Joule, Clausius, Maxwell and Boltzmann etc. and represents dynamic particle or microscopic model        for different gases since it throws light on the behaviour of the particles (atoms and molecules) which constitute the gases and cannot be seen. Properties of gases which we studied earlier are part of macroscopic model.   (2) Postulates   (i) Every gas consists of a large number of small particles called molecules moving with very high velocities in all possible directions.   (ii) The volume of the individual molecule is negligible as compared to the total volume of the gas.   (iii) Gaseous molecules are perfectly elastic so that there is no net loss of kinetic energy due to their collisions.   (iv) The effect of gravity on the motion of the molecules is negligible.   (v) Gaseous molecules are considered as point masses because they do not posses potential energy. So the attractive and repulsive forces between the gas molecules are negligible.   (vi) The pressure of a gas is due to the continuous bombardment on the walls of the containing vessel.   (vii) At constant temperature the average K.E. of all gases is same.   (viii) The average K.E. of the gas molecules is directly proportional to the absolute temperature.   (3) Kinetic gas equation : On the basis of above postulates, the following gas equation was derived,   \[PV=\frac{1}{3}mnu_{rms}^{2}\]   where, P = pressure exerted by the gas   V = volume of the gas   m = average mass of each molecule   n = number of molecules   u = root mean square (RMS) velocity of the gas.   (4) Calculation of kinetic energy   We know that,   K.E. of one molecule\[=\frac{1}{2}m{{u}^{2}}\]   K.E. of n molecules \[=\frac{1}{2}mn{{u}^{2}}=\frac{3}{2}PV\] \[(\because \ \ PV=\frac{1}{3}\ mn{{u}^{2}})\]   n = 1, Then K.E. of 1 mole gas \[=\frac{3}{2}RT\]         \[(\because PV=RT)\]    \[=\frac{3}{2}\times 8.314\times T=12.47\,T\,Joules\].   \[=\frac{\text{Average K}\text{.E}\text{. per mole}}{N(\text{Avogadro number})}=\frac{3}{2}\frac{RT}{N}=\frac{3}{2}KT\] \[\left( K=\frac{R}{N}=\text{Boltzmann constant} \right)\]   This equation shows that K.E. of translation of a gas depends only on the absolute temperature. This is known as Maxwell generalisation. Thus average K.E. \[\propto \,\,T\].   If \[T=0K\] (i.e., \[-{{273.15}^{o}}C)\] then, average K.E. = 0. Thus, absolute zero (0K) is the temperature at which molecular motion ceases.    

(1) Diffusion is the process of spontaneous spreading and intermixing of gases to form homogenous mixture irrespective of force of gravity. While Effusion is the escape of gas molecules through a tiny hole such as pinhole in a balloon.  
  • All gases spontaneously diffuse into one another when they are brought into contact.
 
  • Diffusion into a vacuum will take place much more rapidly than diffusion into another place.
 
  • Both the rate of diffusion of a gas and its rate of effusion depend on its molar mass. Lighter gases diffuses faster than heavier gases. The gas with highest rate of diffusion is hydrogen.
  (2) According to this law, “At constant pressure and temperature, the rate of diffusion or effusion of a gas is inversely proportional to the square root of its vapour density.”   Thus, rate of diffusion \[(r)\propto \frac{1}{\sqrt{d}}\]    (T and P constant)   For two or more gases at constant pressure and temperature, \[\frac{{{r}_{1}}}{{{r}_{2}}}=\sqrt{\frac{{{d}_{2}}}{{{d}_{1}}}}\]   (3) Graham's law can be modified in a number of ways as,   (i) Since, 2 ´ vapour density (V.D.) = Molecular weight   then, \[\frac{{{r}_{1}}}{{{r}_{2}}}=\sqrt{\frac{{{d}_{2}}}{{{d}_{1}}}}=\sqrt{\frac{{{d}_{2}}\times 2}{{{d}_{1}}\times 2}}=\sqrt{\frac{{{M}_{2}}}{{{M}_{1}}}}\]   where, \[{{M}_{1}}\] and \[{{M}_{2}}\] are the molecular weights of the two gases.   (ii)  Since, rate of diffusion \[(r)=\frac{\text{Volume of a gas diffused}}{\text{Time taken for diffusion}}\]then, \[\frac{{{r}_{1}}}{{{r}_{2}}}=\frac{{{V}_{1}}/{{t}_{1}}}{{{V}_{2}}/{{t}_{2}}}=\frac{{{w}_{1}}/{{t}_{1}}}{{{w}_{2}}/{{t}_{2}}}=\sqrt{\frac{{{d}_{2}}}{{{d}_{1}}}}\]   (a) When equal volume of the two gases diffuse, i.e. \[{{V}_{1}}={{V}_{2}}\] then, \[\frac{{{r}_{1}}}{{{r}_{2}}}=\frac{{{t}_{2}}}{{{t}_{1}}}=\sqrt{\frac{{{d}_{2}}}{{{d}_{1}}}}\]   (b) When volumes of the two gases diffuse in the same time, i.e. \[{{t}_{1}}={{t}_{2}}\] then, \[\frac{{{r}_{1}}}{{{r}_{2}}}=\frac{{{V}_{1}}}{{{V}_{2}}}=\sqrt{\frac{{{d}_{2}}}{{{d}_{1}}}}\]   (iii) Since, \[r\propto p\]        (when p is not constant) then, \[\frac{{{r}_{1}}}{{{r}_{2}}}=\frac{{{P}_{1}}}{{{P}_{2}}}\ \sqrt{\frac{{{M}_{2}}}{{{M}_{1}}}}\]            \[\left( \because r\propto \frac{P}{\sqrt{M}} \right)\]   (4) Rate of diffusion and effusion can be determined as,   (i) Rate of diffusion is equal to distance travelled by gas per unit time through a tube of uniform cross-section. (ii)  Number of moles effusing per unit time is also called rate of diffusion. (iii) Decrease in pressure of a cylinder per unit time is called rate of effusion of gas. (iv) The volume of gas effused through a given surface per unit time is also called rate of effusion.   (5) Applications : Graham's law has been used as follows,   (i) To determine vapour densities and molecular weights of gases.   (ii) To prepare Ausell’s marsh gas indicator, used in mines.   (iii) Atmolysis : The process of separation of two gases on the basis of their different rates of diffusion due to difference in their densities is called atmolysis. It has been applied with success for the separation of isotopes and other gaseous mixtures.    

(1) According to this law, “When two or more gases, which do not react chemically are kept in a closed vessel, the total pressure exerted by the mixture is equal to the sum of the partial pressures of individual gases.”   Thus, \[{{P}_{\text{total}}}={{P}_{1}}+{{P}_{2}}+{{P}_{3}}+.........\]   Where \[{{P}_{1}},\,{{P}_{2}},\,{{P}_{3}},......\] are partial pressures of gas number 1, 2, 3 .........   (2) Partial pressure is the pressure exerted by a gas when it is present alone in the same container and at the same temperature.   Partial pressure of a gas \[({{P}_{1}})=\frac{\text{Number of moles of the gas (}{{n}_{1}}\text{)}\times {{P}_{\text{Total}}}}{\text{Total number of moles (}n\text{) in the mixture}}=\text{Mole fraction (}{{X}_{1}}\text{)}\times {{P}_{\text{Total}}}\]   (3) If a number of gases having volume \[{{V}_{1}},\,{{V}_{2}},\,{{V}_{3}}......\] at pressure \[{{P}_{1}},\,{{P}_{2}},\,{{P}_{3}}........\] are mixed together in container of volume V, then,   \[{{P}_{\text{Total}}}=\frac{{{P}_{1}}{{V}_{1}}+{{P}_{2}}{{V}_{2}}+{{P}_{3}}{{V}_{3}}.....}{V}\]   or        \[=({{n}_{1}}+{{n}_{2}}+{{n}_{3}}.....)\frac{RT}{V}\]                \[(\because PV=nRT)\]    or        \[=n\frac{RT}{V}\]    \[(\because n={{n}_{1}}+{{n}_{2}}+{{n}_{3}}.....)\]   (4) Applications : This law is used in the calculation of following relationships,   (i) Mole fraction of a gas \[({{X}_{1}})\] in a mixture of gas \[=\frac{\text{Partial pressure of a gas (}{{P}_{1}}\text{)}}{{{P}_{\text{Total}}}}\]   (ii) % of a gas in mixture \[=\frac{\text{Partial pressure of a gas }({{P}_{1}})}{{{P}_{\text{Total}}}}\times 100\]   (iii) Pressure of dry gas collected over water : When a gas is collected over water, it becomes moist due to water vapour which exerts its own partial pressure at the same temperature of the gas. This partial perssure of water vapours is called aqueous tension. Thus,  \[{{P}_{\text{dry gas}}}={{P}_{\text{moist gas}}}\text{ or }{{P}_{\text{Total}}}-{{P}_{\text{water vapour}}}\]   or \[{{P}_{\text{dry gas}}}={{P}_{\text{moist}\ \text{gas}}}-\] Aqueous tension (Aqueous tension is directly proportional to absolute temperature)   (iv) Relative humidity (RH) at a given temperature is given by,     \[RH=\frac{\text{Partial pressure of water in air}}{\text{Vapour pressure of water}}\].   (5) Limitations : This law is applicable only when the component gases in the mixture do not react with each other. For example, \[{{N}_{2}}\] and \[{{O}_{2}}\], CO  and \[C{{O}_{2}}\], \[{{N}_{2}}\] and \[C{{l}_{2}}\], CO and \[{{N}_{2}}\] etc. But this law is not applicable to gases which combine chemically. For example, \[{{H}_{2}}\] and \[C{{l}_{2}}\], CO and \[C{{l}_{2}}\], \[N{{H}_{3}}\], HBr and HCl, NO and \[{{O}_{2}}\] etc.   (6) Another law, which is really equivalent to the law of partial pressures and related to the partial volumes of gases is known as Law of partial volumes given by Amagat. According to this law, “When two or more gases, which do not react chemically are kept in a closed vessel, the total volume exerted by the mixture is equal to the sum of the partial volumes of individual gases.”   Thus, \[{{V}_{\text{Total}}}={{V}_{1}}+{{V}_{2}}+{{V}_{3}}+......\]   Where \[{{V}_{1}},\,{{V}_{2}},\,{{V}_{3}},......\] are partial volumes of gas number 1, 2, 3.....    

(1) The simple gas laws relating gas volume to pressure, temperature and amount of gas, respectively, are stated below :   Boyle's law :        \[P\propto \frac{1}{V}\] or \[V\propto \frac{1}{P}\]            (n and T constant)   Charle's law :      \[V\propto \text{T}\]                 (n and P constant)   Avogadro's law : \[V\propto n\]                           (T and P constant)   If all the above law's combines, then                                           \[V\propto \frac{nT}{P}\]   or               \[V=\frac{nRT}{P}\] (\[R=\] Ideal gas constant)   or            \[PV=nRT\]   This is called ideal gas equation. R is called ideal gas constant. This equation is obeyed by isothermal and adiabatic processes.   (2) Nature and values of R : From the ideal gas equation, \[R=\frac{PV}{nT}=\frac{\text{Pressure}\times \text{Volume}}{\text{mole}\times \text{Temperature}}\]   \[=\frac{\frac{\text{Force}}{\text{Area}}\times \text{Volume}}{\text{mole}\times \text{Temperature}}=\frac{\text{Force}\times \text{Length}}{\text{mole}\times \text{Temperature}}\]\[=\frac{\text{Work or energy}}{\text{mole}\times \text{Temperature}}\].   R is expressed in the unit of work or energy \[mo{{l}^{-1}}\,{{K}^{-1}}\].   Since different values of R are summarised below :   \[R=0.0821\,L\,atm\,mo{{l}^{-1}}\,{{K}^{-1}}\]   \[=8.3143\,joule\,mo{{l}^{-1}}\,{{K}^{-1}}\]  (S.I. unit)   \[=8.3143\,Nm\,mo{{l}^{-1}}\,{{K}^{-1}}\]    \[=8.3143\,KPa\,d{{m}^{3}}\,mo{{l}^{-1}}\,{{K}^{-1}}\]   \[=8.3143\,MPa\,c{{m}^{3}}\,mo{{l}^{-1}}\,{{K}^{-1}}\]   \[=5.189\times {{10}^{19}}\,eV\,mo{{l}^{-1}}\,{{K}^{-1}}\]   \[=1.99\,cal\,mo{{l}^{-1}}\,{{K}^{-1}}\]   (3) Gas constant, R for a single molecule is called Boltzmann constant (k)   \[k=\frac{R}{N}=\frac{8.314\times {{10}^{7}}}{6.023\times {{10}^{23}}}ergs\,mol{{e}^{-1}}\,degre{{e}^{-1}}\]   \[=1.38\times {{10}^{-16}}ergs\,mo{{l}^{-1}}\,degre{{e}^{-1}}\]   or \[1.38\times {{10}^{-23}}\,joule\,mo{{l}^{-1}}\,degre{{e}^{-1}}\]     (4) Calculation of mass, molecular weight and density of the gas by gas equation   \[PV=nRT=\frac{m}{M}RT\]        \[\left( \because n=\frac{\text{mass of the gas (}m\text{)}}{\text{Molecular weight of the gas (}M\text{)}} \right)\]   \[\therefore \]  \[M=\frac{mRT}{PV}\]         \[d=\frac{PM}{RT}\]                            \[\left( \because d=\frac{m}{V} \right)\]   or        \[\frac{dT}{P}=\frac{M}{R}\], \[\frac{M}{R}=\] Constant   (\[\because \] M and R are constant for a particular gas)   Thus, \[\frac{dT}{P}\] or \[\frac{{{d}_{1}}{{T}_{1}}}{{{P}_{1}}}=\frac{{{d}_{2}}{{T}_{2}}}{{{T}_{2}}}\]= Constant    (For two or more different temperature and pressure)   (5) Gas densities differ from those of solids and liquids as,   (i)        Gas densities are generally stated in g/L instead of \[g/c{{m}^{3}}\].   (ii)       Gas densities are strongly dependent on pressure and temperature as, \[d\propto P\]\[\propto 1/T\]   Densities of liquids and solids, do depend somewhat on temperature, but they are far less dependent on pressure.   (iii) The density of a gas is directly proportional to its molar mass. No simple relationship exists between the density and molar mass for liquid and solids.   (iv) Density of a gas at STP \[=\frac{\text{molar mass}}{22.4}\]   \[d({{N}_{2}})\] at STP\[=\frac{28}{22.4}=1.25\,g\,{{L}^{-1}}\],   \[d({{O}_{2}})\] at STP \[=\frac{32}{22.4}=1.43\,g\,{{L}^{-1}}\]

(1) According to this law, “Equal volumes of any two gases at the same temperature and pressure contain the same number of molecules.”   Thus, \[V\propto n\]              (at constant T and P)   or \[V=Kn\]            (where K is constant)   or \[\frac{{{V}_{1}}}{{{n}_{1}}}=\frac{{{V}_{2}}}{{{n}_{2}}}=.......=K\]   Example,                 \[\underset{1n\,litre}{\mathop{\underset{1\,litre}{\mathop{\underset{2\,litres}{\mathop{\underset{2\,volumes}{\mathop{\underset{2\,moles}{\mathop{2{{H}_{2}}(g)}}\,}}\,}}\,}}\,}}\,+\underset{1/2n\,litre}{\mathop{\underset{1/2\,litre}{\mathop{\underset{1\,litre}{\mathop{\underset{1\,volume}{\mathop{\underset{1\,mole}{\mathop{{{O}_{2}}(g)}}\,}}\,}}\,}}\,}}\,\xrightarrow{{}}\underset{1n\,litre}{\mathop{\underset{1\,litre}{\mathop{\underset{2\,litres}{\mathop{\underset{2\,volumes}{\mathop{\underset{2\,moles}{\mathop{2{{H}_{2}}O(g)}}\,}}\,}}\,}}\,}}\,\]   (2) One mole of any gas contains the same number of molecules (Avogadro's number \[=6.02\times {{10}^{23}}\]) and by this law must occupy the same volume at a given temperature and pressure. The volume of one mole of a gas is called molar volume, Vm which is 22.4 L \[mo{{l}^{-1}}\] at S.T.P. or N.T.P.   (3) This law can also express as, “The molar gas volume at a given temperature and pressure is a specific constant independent of the nature of the gas”.   Thus, \[{{V}_{m}}=\] specific constant \[=22.4\,L\,mo{{l}^{-1}}\] at S.T.P. or N.T.P.  

(1) In 1802, French chemist Joseph Gay-Lussac studied the variation of pressure with temperature and extende the Charle’s law so, this law is also called Charle’s-Gay Lussac’s law.   (2) It states that, “The pressure of a given mass of a gas is directly proportional to the absolute temperature \[(={{\,}^{o}}C+273)\] at constant volume.”   Thus, \[P\propto T\] at constant volume and mass   or \[P=KT=K(t{{(}^{o}}C)+273.15)\]          (where K is constant)   \[K=\frac{P}{T}\] or \[\frac{{{P}_{1}}}{{{T}_{1}}}=\frac{{{P}_{2}}}{{{T}_{2}}}=K\] (For two or more gases)   (3) If \[t={{0}^{o}}C\], then \[P={{P}_{0}}\]   Hence, \[{{P}_{0}}=K\times 273.15\]   \[\therefore \]   \[K=\frac{{{P}_{0}}}{273.15}\]              \[P=\frac{{{P}_{0}}}{273.15}[t+273.15]={{P}_{0}}\left[ 1+\frac{t}{273.15} \right]={{P}_{0}}[1+\alpha t]\]   where \[{{\alpha }_{P}}\] is the pressure coefficient,   \[{{\alpha }_{P}}=\frac{P-{{P}_{0}}}{t{{P}_{0}}}=\frac{1}{273.15}=3.661\times {{10}^{-3}}{{\,}^{o}}{{C}^{-1}}\]   Thus, for every \[{{1}^{o}}\] change in temperature, the pressure of a gas changes by \[\frac{1}{273.15}\left( \approx \frac{1}{273} \right)\] of the pressure at \[{{0}^{o}}C\].   (4) This law fails at low temperatures, because the volume of the gas molecules be come significant.   (5) Graphical representation of Gay-Lussac's law : A graph between P and T at constant V is called isochore.      


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