Comprehensive Study Guide on Chemical Quantities, Rotational Kinematics, and Mechanical Work and Power

Physical Quantities Related to Amount of Substance

  • Fundamental Conversions and Reference Standards:

    • Mass Conversions:

      • 1 kg=103 g1\,\text{kg} = 10^3\,\text{g}

      • 1 mg=10−3 g1\,\text{mg} = 10^{-3}\,\text{g}

    • Volume Conversions:

      • 1 L=10−3 m31\,\text{L} = 10^{-3}\,\text{m}^3

      • 1 L=1 dm31\,\text{L} = 1\,\text{dm}^3

      • 1 mL=10−3 L1\,\text{mL} = 10^{-3}\,\text{L}

      • 1 cm3=1 mL=10−3 L1\,\text{cm}^3 = 1\,\text{mL} = 10^{-3}\,\text{L}

      • Conversion between molar volume units: to convert from m3⋅mol−1\text{m}^3\cdot\text{mol}^{-1} to L⋅mol−1\text{L}\cdot\text{mol}^{-1}, multiply by 10−310^{-3}.

    • Volumetric Mass (Density) Conversions:

      • 1 g/cm3=103 kg/m31\,\text{g/cm}^3 = 10^3\,\text{kg/m}^3

      • 1 g/cm3=1 g/mL1\,\text{g/cm}^3 = 1\,\text{g/mL}

    • Pressure Conversions:

      • 1 atm=1.013×105 Pa1\,\text{atm} = 1.013 \times 10^5\,\text{Pa}

      • 1 bar=105 Pa1\,\text{bar} = 10^5\,\text{Pa}

      • 1 hPa=102 Pa1\,\text{hPa} = 10^2\,\text{Pa}

      • 1 kPa=103 Pa1\,\text{kPa} = 10^3\,\text{Pa}

      • 1 atm=76 cmHg=760 mmHg1\,\text{atm} = 76\,\text{cmHg} = 760\,\text{mmHg}

    • Absolute Temperature Conversion:

      • T(K)=θ(∘C)+273.15T(\text{K}) = \theta(^\circ\text{C}) + 273.15

    • Substance Quantity Conversions:

      • 1 mmol=10−3 mol1\,\text{mmol} = 10^{-3}\,\text{mol}

  • Definition and Relations of the Amount of Substance (nn):

    • The amount of substance n(X)n(X) represents the chemical quantity of an elementary entity XX, expressed in moles (mol\text{mol}).

    • General Master Relationship:         n(X)=NNA=m(X)M(X)=V(X)Vm=C×Vn(X) = \frac{N}{N_A} = \frac{m(X)}{M(X)} = \frac{V(X)}{V_m} = C \times V

    • Definition of Variables and Units:

      • NN: Total number of microscopic entities or constituents (dimensionless).

      • NAN_A: Avogadro's constant, defined as NA=6.03×1023 mol−1N_A = 6.03 \times 10^{23}\,\text{mol}^{-1}.

      • m(X)m(X): Mass of sample XX, expressed in grams (g\text{g}).

      • M(X)M(X): Molar mass of entity XX, expressed in grams per mole (g⋅mol−1\text{g}\cdot\text{mol}^{-1}).

      • V(X)V(X): Volume occupied by gaseous species XX, expressed in liters (L\text{L}).

      • VmV_m: Molar volume of a gas under given temperature and pressure conditions, expressed in liters per mole (L⋅mol−1\text{L}\cdot\text{mol}^{-1}).

      • CC: Molar concentration of solute in solution, expressed in moles per liter (mol⋅L−1\text{mol}\cdot\text{L}^{-1}).

      • VV: Volume of the solution or gas sample, expressed in liters (L\text{L}).

  • Molar Mass Determinations:

    • Standard Atomic Molar Masses (g⋅mol−1\text{g}\cdot\text{mol}^{-1}):

      • Hydrogen (H\text{H}): M(H)=1 g⋅mol−1M(\text{H}) = 1\,\text{g}\cdot\text{mol}^{-1}

      • Helium (He\text{He}): M(He)=4 g⋅mol−1M(\text{He}) = 4\,\text{g}\cdot\text{mol}^{-1}

      • Carbon (C\text{C}): M(C)=12 g⋅mol−1M(\text{C}) = 12\,\text{g}\cdot\text{mol}^{-1}

      • Nitrogen (N\text{N}): M(N)=14 g⋅mol−1M(\text{N}) = 14\,\text{g}\cdot\text{mol}^{-1}

      • Oxygen (O\text{O}): M(O)=16 g⋅mol−1M(\text{O}) = 16\,\text{g}\cdot\text{mol}^{-1}

      • Fluorine (F\text{F}): M(F)=19 g⋅mol−1M(\text{F}) = 19\,\text{g}\cdot\text{mol}^{-1}

      • Sulfur (S\text{S}): M(S)=32 g⋅mol−1M(\text{S}) = 32\,\text{g}\cdot\text{mol}^{-1}

      • Iron (Fe\text{Fe}): M(Fe)=56 g⋅mol−1M(\text{Fe}) = 56\,\text{g}\cdot\text{mol}^{-1}

      • Copper (Cu\text{Cu}): M(Cu)=63.5 g⋅mol−1M(\text{Cu}) = 63.5\,\text{g}\cdot\text{mol}^{-1}

      • Zinc (Zn\text{Zn}): M(Zn)=65.4 g⋅mol−1M(\text{Zn}) = 65.4\,\text{g}\cdot\text{mol}^{-1}

      • Silver (Ag\text{Ag}): M(Ag)=108 g⋅mol−1M(\text{Ag}) = 108\,\text{g}\cdot\text{mol}^{-1}

    • Molecular Molar Mass Calculation Examples:

      • Water (H2O\text{H}_2\text{O}):             M(H2O)=2×M(H)+M(O)=2×1+16=18 g⋅mol−1M(\text{H}_2\text{O}) = 2 \times M(\text{H}) + M(\text{O}) = 2 \times 1 + 16 = 18\,\text{g}\cdot\text{mol}^{-1}

      • Glucose (C6H12O6\text{C}_6\text{H}_{12}\text{O}_6):             M(C6H12O6)=6×M(C)+12×M(H)+6×M(O)M(\text{C}_6\text{H}_{12}\text{O}_6) = 6 \times M(\text{C}) + 12 \times M(\text{H}) + 6 \times M(\text{O})             M(C6H12O6)=6×12+12×1+6×16=72+12+96=180 g⋅mol−1M(\text{C}_6\text{H}_{12}\text{O}_6) = 6 \times 12 + 12 \times 1 + 6 \times 16 = 72 + 12 + 96 = 180\,\text{g}\cdot\text{mol}^{-1}

  • Molar Volume of Gases (VmV_m):

    • Definition: The molar volume is the volume occupied by one mole of any gas at a specified pressure PP and temperature TT.

    • Thermodynamic Formula:         Vm=R×TPV_m = \frac{R \times T}{P}         where R=8.314 S.I.R = 8.314\,\text{S.I.}, TT is in Kelvin (K\text{K}), and PP is in Pascals (Pa\text{Pa}).

    • Standard Conditions for Temperature and Pressure (CSTP):

      • Temperature: T=20 ∘CT = 20\,^\circ\text{C}

      • Pressure: P=1 atmP = 1\,\text{atm}

      • Resulting Molar Volume: Vm=24 L⋅mol−1V_m = 24\,\text{L}\cdot\text{mol}^{-1}

    • Normal Conditions for Temperature and Pressure (CNTP):

      • Temperature: T=0 ∘CT = 0\,^\circ\text{C}

      • Pressure: P=1 atmP = 1\,\text{atm}

      • Resulting Molar Volume: Vm=22.4 L⋅mol−1V_m = 22.4\,\text{L}\cdot\text{mol}^{-1}

  • Density, Relative Density, and Concentrations:

    • Volumetric Mass (Density ρ\rho):         ρ=mV\rho = \frac{m}{V}         where mm is the mass in grams (g\text{g}), VV is the volume in cubic centimeters (cm3\text{cm}^3), and ρ\rho is expressed in g⋅cm−3\text{g}\cdot\text{cm}^{-3}.

    • Relative Density of a Condensed Body (Liquid or Solid) relative to Water (dd):         d=ρρ0d = \frac{\rho}{\rho_0}         where ρ0\rho_0 is the volumetric mass of water, with a standard value of ρ0=1 g⋅cm−3=1 g⋅mL−1\rho_0 = 1\,\text{g}\cdot\text{cm}^{-3} = 1\,\text{g}\cdot\text{mL}^{-1}.         ρ=d×ρ0\rho = d \times \rho_0

    • Relative Density of a Gas relative to Air (dd):         d=M(X)29d = \frac{M(X)}{29}         where M(X)M(X) is the molar mass of the gaseous species expressed in g⋅mol−1\text{g}\cdot\text{mol}^{-1}, and 29 g⋅mol−129\,\text{g}\cdot\text{mol}^{-1} represents the equivalent molar mass of atmospheric air.

    • Molar Concentration (CC):         C=n(X)V=m(X)M(X)×VC = \frac{n(X)}{V} = \frac{m(X)}{M(X) \times V}         expressed in mol⋅L−1\text{mol}\cdot\text{L}^{-1}.

    • Mass Concentration (CmC_m):         Cm=m(X)V=n(X)×M(X)VC_m = \frac{m(X)}{V} = \frac{n(X) \times M(X)}{V}         expressed in g⋅L−1\text{g}\cdot\text{L}^{-1}.

    • Interrelation between Molar and Mass Concentration:         C=CmM(X)C = \frac{C_m}{M(X)}         Cm=C×M(X)C_m = C \times M(X)

    • Relationship between Amount of Substance n(X)n(X) and Relative Density dd:         m(X)=ρ×V=d×ρ0×Vm(X) = \rho \times V = d \times \rho_0 \times V         n(X)=ρ×VM(X)=d×ρ0×VM(X)n(X) = \frac{\rho \times V}{M(X)} = \frac{d \times \rho_0 \times V}{M(X)}         where VV is expressed in mL\text{mL} when using ρ0=1 g⋅mL−1\rho_0 = 1\,\text{g}\cdot\text{mL}^{-1}.

    • Relationship between Molar Concentration CC and Relative Density dd:         C=n(X)V=ρM(X)=d×ρ0M(X)C = \frac{n(X)}{V} = \frac{\rho}{M(X)} = \frac{d \times \rho_0}{M(X)}

    • Mass Percentage (PP):

      • The mass percentage PP denotes the mass fraction of a pure chemical species XX contained within a solution of total mass msm_s:             m(X)=P×ms=P×ρs×Vs=P×d×ρ0×Vsm(X) = P \times m_s = P \times \rho_s \times V_s = P \times d \times \rho_0 \times V_s

      • The resulting molar concentration CC of the solution is given by:             C=m(X)M(X)×Vs=P×d×ρ0M(X)C = \frac{m(X)}{M(X) \times V_s} = \frac{P \times d \times \rho_0}{M(X)}

  • Gas Laws:

    • Ideal Gas Equation of State:         P×V=n(X)×R×TP \times V = n(X) \times R \times T

      • International System of Units (SI):

        • Pressure: PP in Pascals (Pa\text{Pa})

        • Volume: VV in cubic meters (m3\text{m}^3)

        • Amount of substance: n(X)n(X) in moles (mol\text{mol})

        • Universal gas constant: R=8.314 J⋅mol−1⋅K−1R = 8.314\,\text{J}\cdot\text{mol}^{-1}\cdot\text{K}^{-1} (or S.I.\text{S.I.})

        • Absolute temperature: TT in Kelvin (K\text{K})

      • Alternative Practical Units:

        • Pressure: PP in atmospheres (atm\text{atm})

        • Volume: VV in liters (L\text{L})

        • Universal gas constant: R=0.082 L⋅atm⋅mol−1⋅K−1R = 0.082\,\text{L}\cdot\text{atm}\cdot\text{mol}^{-1}\cdot\text{K}^{-1}

    • Boyle-Mariotte's Law:

      • Applies to an ideal gas undergoing an isothermal transformation (where temperature TT remains strictly constant):             P1×V1=P2×V2=constantP_1 \times V_1 = P_2 \times V_2 = \text{constant}

Kinematics of Rotational Motion of a Rigid Solid Around a Fixed Axis

  • Positional Kinematic Quantities:

    • Curvilinear Abscissa (s(t)s(t)):

      • Defined as the algebraic arc length along the circular trajectory traced by point MM from an initial reference point M0M_0 at time t0t_0:             s(t)=M0M⌢s(t) = \overset{\frown}{M_0 M}

      • Unit: meters (m\text{m}).

    • Angular Abscissa (θ(t)\theta(t)):

      • Defined as the oriented angle formed between the reference radius vector OM0⃗\vec{OM_0} and the instantaneous radius vector OM⃗\vec{OM}:             θ(t)=(OM0⃗,OM⃗)\theta(t) = (\vec{OM_0}, \vec{OM})

      • Unit: radians (rad\text{rad}).

    • Geometric Relation:         s=R×θs = R \times \theta         where RR is the radius of the circular trajectory traced by point MM.

  • Linear and Angular Velocities:

    • Linear Velocity (vv):

      • Average Linear Velocity (vv): Calculated between two positions M1M_1 and M2M_2 over a time interval Δt\Delta t:             v=M1M2Δtv = \frac{M_1 M_2}{\Delta t}             expressed in m⋅s−1\text{m}\cdot\text{s}^{-1}.

      • Instantaneous Linear Velocity (viv_i): Calculated at recorded position MiM_i using neighboring positions:             vi=Mi−1Mi+12×τv_i = \frac{M_{i-1} M_{i+1}}{2 \times \tau}             where τ\tau is the constant time interval between consecutive recordings (Δt=2×τ\Delta t = 2 \times \tau).

    • Angular Velocity (ω\omega):

      • Average Angular Velocity (ω\omega): Calculated over an angular displacement Δθ\Delta \theta across elapsed time Δt\Delta t:             ω=ΔθΔt\omega = \frac{\Delta \theta}{\Delta t}             expressed in rad⋅s−1\text{rad}\cdot\text{s}^{-1}.

      • Instantaneous Angular Velocity (ωi\omega_i): Calculated at recording instant tit_i using adjacent angular measurements:             ωi=θi+1−θi−12×τ\omega_i = \frac{\theta_{i+1} - \theta_{i-1}}{2 \times \tau}

    • Kinematic Relationship between Linear and Angular Velocity:         v=R×ωv = R \times \omega

  • Uniform Rotational Motion:

    • Definition: A rotational motion is defined as uniform when the instantaneous angular velocity remains constant over time:         ω0=ΔθΔt=constant\omega_0 = \frac{\Delta \theta}{\Delta t} = \text{constant}

    • Period (TT):

      • The time duration required for the solid to execute one complete revolution (1 turn1\,\text{turn}):             T=2×πω0T = \frac{2 \times \pi}{\omega_0}

      • Unit: seconds (s\text{s}).

    • Frequency (ff or NN):

      • The number of complete revolutions executed per unit time (per second):             f=N=1T=ω02×πf = N = \frac{1}{T} = \frac{\omega_0}{2 \times \pi}

      • Unit: Hertz (Hz\text{Hz}).

    • Angular Displacement and Total Number of Turns (nn):         Δθ=θ2−θ1\Delta \theta = \theta_2 - \theta_1         Δθ=2×π×n\Delta \theta = 2 \times \pi \times n         where nn denotes the total number of full revolutions performed during the interval.

    • Time Equations of Motion (Lois Horaires):

      • Angular Abscissa Time Law:             θ(t)=ω0×t+θ0\theta(t) = \omega_0 \times t + \theta_0             where θ0\theta_0 is the initial angular position at t=0 st = 0\,\text{s}. The plot of θ(t)\theta(t) against tt yields a straight line with slope equal to ω0\omega_0 and vertical intercept θ0\theta_0.

      • Curvilinear Abscissa Time Law:             s(t)=v×t+s0s(t) = v \times t + s_0             where s0s_0 is the initial curvilinear position at t=0 st = 0\,\text{s}.

Work and Power of Mechanical Forces

  • General Concepts and Work Expressions:

    • Mechanical work represents the energy transferred to or from an object via the application of a force along a displacement. Unit: Joules (J\text{J}).

    • Work of a Constant Force in Rectilinear Translation:

      • For a constant force F⃗\vec{F} acting during a straight displacement from point AA to point BB:             WA→B(F⃗)=F×AB×cos⁡(α)W_{A \rightarrow B}(\vec{F}) = F \times AB \times \cos(\alpha)             where FF is the magnitude of the force in Newtons (N\text{N}), ABAB is the displacement distance in meters (m\text{m}), and α\alpha is the angle between force vector F⃗\vec{F} and displacement vector AB⃗\vec{AB}.

    • Work of a Force in Rotation Around a Fixed Axis (Δ\Delta):

      • For a force exerting a rotational effect about axis Δ\Delta over an angular displacement Δθ\Delta \theta:             WA→B(F⃗)=MΔ(F⃗)×ΔθW_{A \rightarrow B}(\vec{F}) = \mathcal{M}_\Delta(\vec{F}) \times \Delta \theta             where MΔ(F⃗)\mathcal{M}_\Delta(\vec{F}) is the moment of force F⃗\vec{F} with respect to axis Δ\Delta in N⋅m\text{N}\cdot\text{m}, and Δθ\Delta \theta is in radians (rad\text{rad}).

    • Physical Classification of Work Based on Sign:

      • W>0W > 0: Motive work (travail moteur), occurring when cos⁡(α)>0\cos(\alpha) > 0 (0≤α<π20 \le \alpha < \frac{\pi}{2}), supplying mechanical energy to the system.

      • W<0W < 0: Resistive work (travail résistant), occurring when cos⁡(α)<0\cos(\alpha) < 0 (π2<α≤π\frac{\pi}{2} < \alpha \le \pi), removing mechanical energy from the system.

      • W=0W = 0: Null work (travail nul), occurring when cos⁡(α)=0\cos(\alpha) = 0 (α=π2\alpha = \frac{\pi}{2}), where the force vector is perpendicular to displacement.

  • Work Done by the Gravitational Force (Weight P⃗\vec{P}):

    • General Path-Independent Formulation:         W(P⃗)=m×g×(zi−zf)W(\vec{P}) = m \times g \times (z_i - z_f)

      • During downward motion (descent, where zi>zfz_i > z_f):             W(P⃗)=+m×g×hW(\vec{P}) = +m \times g \times h

      • During upward motion (ascent, where zi<zfz_i < z_f):             W(P⃗)=−m×g×hW(\vec{P}) = -m \times g \times h         where h=∣zi−zf∣h = |z_i - z_f| is the vertical altitude variation.

    • Specific Trajectory Configurations:

      • Horizontal Displacement from AA to BB:             WA→B(P⃗)=0 JW_{A \rightarrow B}(\vec{P}) = 0\,\text{J}             because the weight vector P⃗\vec{P} is orthogonal to the horizontal displacement vector AB⃗\vec{AB}.

      • Straight Inclined Plane (Descent from AA to BB at Angle α\alpha to Horizontal):             The vertical drop is h=AB×sin⁡(α)h = AB \times \sin(\alpha), yielding:             WA→B(P⃗)=+m×g×AB×sin⁡(α)W_{A \rightarrow B}(\vec{P}) = +m \times g \times AB \times \sin(\alpha)

      • Straight Inclined Plane (Ascent from BB to AA at Angle α\alpha to Horizontal):             WB→A(P⃗)=−m×g×AB×sin⁡(α)W_{B \rightarrow A}(\vec{P}) = -m \times g \times AB \times \sin(\alpha)

      • Circular Concave Trajectory of Radius R=OAR = OA (Descent from AA to Equilibrium Position BB):             For an arc subtending angle α\alpha from the vertical equilibrium axis:             h=R−R×cos⁡(α)=R×(1−cos⁡(α))h = R - R \times \cos(\alpha) = R \times (1 - \cos(\alpha))             WA→B(P⃗)=+m×g×R×(1−cos⁡(α))W_{A \rightarrow B}(\vec{P}) = +m \times g \times R \times (1 - \cos(\alpha))

  • Work Done by the Contact Surface Reaction Force (R⃗\vec{R}):

    • Motion Without Friction (Sans frottement):

      • The reaction force R⃗\vec{R} remains strictly normal (perpendicular) to the contact surface (R⃗=R⃗N\vec{R} = \vec{R}_N and R⃗⊥AB⃗\vec{R} \perp \vec{AB}):             W(R⃗)=0 JW(\vec{R}) = 0\,\text{J}

    • Motion With Friction (Avec frottement):

      • The reaction force tilts opposite the direction of motion and decomposes into a normal component R⃗N\vec{R}_N and a tangential frictional component R⃗T\vec{R}_T (or f⃗\vec{f}):             R⃗=R⃗N+R⃗T\vec{R} = \vec{R}_N + \vec{R}_T

      • Since R⃗N⊥AB⃗\vec{R}_N \perp \vec{AB}, its work is zero, leaving exclusively the resistive work of friction:             W(R⃗)=W(R⃗T)=−RT×ABW(\vec{R}) = W(\vec{R}_T) = -R_T \times AB

  • Principle of Inertia and Equilibrium Condition:

    • In uniform rectilinear motion, the vector sum of external forces applied to a solid body is zero (Principle of Inertia):         ∑F⃗i=0⃗  ⟹  ∑WA→B(F⃗i)=0\sum \vec{F}_i = \vec{0} \implies \sum W_{A \rightarrow B}(\vec{F}_i) = 0

  • Power of a Force (PP):

    • Mechanical power characterizes the rate at which work is performed per unit time. Unit: Watts (W\text{W}).

    • Average Power (PmP_m):         Pm=W(F⃗)ΔtP_m = \frac{W(\vec{F})}{\Delta t}         where W(F⃗)W(\vec{F}) is the work performed across time interval Δt\Delta t.

    • Instantaneous Power (P(t)P(t)):

      • In Translatory Motion:             P(t)=F⃗⋅v⃗=F×v×cos⁡(F⃗,v⃗)P(t) = \vec{F} \cdot \vec{v} = F \times v \times \cos(\vec{F}, \vec{v})             where v⃗\vec{v} is the instantaneous linear velocity vector.

      • In Rotational Motion:             P(t)=MΔ(F⃗)×ω(t)P(t) = \mathcal{M}_\Delta(\vec{F}) \times \omega(t)             where MΔ(F⃗)\mathcal{M}_\Delta(\vec{F}) is the moment of the force about axis Δ\Delta, and ω(t)\omega(t) is the instantaneous angular velocity in rad⋅s−1\text{rad}\cdot\text{s}^{-1}.