Specific Heat Capacity given heat capacity Solution

STEP 0: Pre-Calculation Summary
Formula Used
Specific Heat Capacity = Heat Capacity/(Mass*Change in Temperature)
c = C/(Massflight path*∆T)
This formula uses 4 Variables
Variables Used
Specific Heat Capacity - (Measured in Joule per Kilogram per K) - Specific Heat Capacity is the heat required to raise the temperature of the unit mass of a given substance by a given amount.
Heat Capacity - (Measured in Joule per Kelvin) - The Heat Capacity is a physical property of matter, defined as the amount of heat to be supplied to a given mass of a material to produce a unit change in its temperature.
Mass - (Measured in Kilogram) - Mass is the quantity of matter in a body regardless of its volume or of any forces acting on it.
Change in Temperature - (Measured in Kelvin) - The Change in Temperature is the difference between the initial and final temperature.
STEP 1: Convert Input(s) to Base Unit
Heat Capacity: 500 Joule per Kelvin --> 500 Joule per Kelvin No Conversion Required
Mass: 35.45 Kilogram --> 35.45 Kilogram No Conversion Required
Change in Temperature: 50 Kelvin --> 50 Kelvin No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
c = C/(Massflight path*∆T) --> 500/(35.45*50)
Evaluating ... ...
c = 0.282087447108604
STEP 3: Convert Result to Output's Unit
0.282087447108604 Joule per Kilogram per K -->0.000282087447108604 Kilojoule per Kilogram per K (Check conversion here)
FINAL ANSWER
0.000282087447108604 0.000282 Kilojoule per Kilogram per K <-- Specific Heat Capacity
(Calculation completed in 00.004 seconds)

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University of Hawaiʻi at Mānoa (UH Manoa), Hawaii, USA
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24 Equipartition Principle and Heat Capacity Calculators

Internal Molar Energy of Non-Linear Molecule
Go Molar Internal Energy = ((3/2)*[R]*Temperature)+((0.5*Moment of Inertia along Y-axis*(Angular Velocity along Y-axis^2))+(0.5*Moment of Inertia along Z-axis*(Angular Velocity along Z-axis^2))+(0.5*Moment of Inertia along X-axis*(Angular Velocity along X-axis^2)))+((3*Atomicity)-6)*([R]*Temperature)
Average Thermal Energy of Non-linear Polyatomic Gas Molecule
Go Thermal Energy = ((3/2)*[BoltZ]*Temperature)+((0.5*Moment of Inertia along Y-axis*(Angular Velocity along Y-axis^2))+(0.5*Moment of Inertia along Z-axis*(Angular Velocity along Z-axis^2)))+((3*Atomicity)-6)*([BoltZ]*Temperature)
Average Thermal Energy of Linear Polyatomic Gas Molecule
Go Thermal Energy = ((3/2)*[BoltZ]*Temperature)+((0.5*Moment of Inertia along Y-axis*(Angular Velocity along Y-axis^2))+(0.5*Moment of Inertia along Z-axis*(Angular Velocity along Z-axis^2)))+((3*Atomicity)-5)*([BoltZ]*Temperature)
Internal Molar Energy of Linear Molecule
Go Molar Internal Energy = ((3/2)*[R]*Temperature)+((0.5*Moment of Inertia along Y-axis*(Angular Velocity along Y-axis^2))+(0.5*Moment of Inertia along Z-axis*(Angular Velocity along Z-axis^2)))+((3*Atomicity)-5)*([R]*Temperature)
Rotational Energy of Non-Linear Molecule
Go Rotational Energy = (0.5*Moment of Inertia along Y-axis*Angular Velocity along Y-axis^2)+(0.5*Moment of Inertia along Z-axis*Angular Velocity along Z-axis^2)+(0.5*Moment of Inertia along X-axis*Angular Velocity along X-axis^2)
Translational Energy
Go Translational Energy = ((Momentum along X-axis^2)/(2*Mass))+((Momentum along Y-axis^2)/(2*Mass))+((Momentum along Z-axis^2)/(2*Mass))
Rotational Energy of Linear Molecule
Go Rotational Energy = (0.5*Moment of Inertia along Y-axis*(Angular Velocity along Y-axis^2))+(0.5*Moment of Inertia along Z-axis*(Angular Velocity along Z-axis^2))
Vibrational Energy Modeled as Harmonic Oscillator
Go Vibrational Energy = ((Momentum of Harmonic Oscillator^2)/(2*Mass))+(0.5*Spring Constant*(Change in Position^2))
Average Thermal Energy of Non-linear polyatomic Gas Molecule given Atomicity
Go Thermal Energy given Atomicity = ((6*Atomicity)-6)*(0.5*[BoltZ]*Temperature)
Average Thermal Energy of Linear Polyatomic Gas Molecule given Atomicity
Go Thermal Energy given Atomicity = ((6*Atomicity)-5)*(0.5*[BoltZ]*Temperature)
Total Kinetic Energy
Go Total Energy = Translational Energy+Rotational Energy+Vibrational Energy
Specific Heat Capacity given heat capacity
Go Specific Heat Capacity = Heat Capacity/(Mass*Change in Temperature)
Internal Molar Energy of Non-Linear Molecule given Atomicity
Go Molar Internal Energy = ((6*Atomicity)-6)*(0.5*[R]*Temperature)
Internal Molar Energy of Linear Molecule given Atomicity
Go Molar Internal Energy = ((6*Atomicity)-5)*(0.5*[R]*Temperature)
Heat Capacity
Go Heat Capacity = Mass*Specific Heat Capacity*Change in Temperature
Molar Vibrational Energy of Non-Linear Molecule
Go Vibrational Molar Energy = ((3*Atomicity)-6)*([R]*Temperature)
Molar Vibrational Energy of Linear Molecule
Go Vibrational Molar Energy = ((3*Atomicity)-5)*([R]*Temperature)
Vibrational Energy of Non-Linear Molecule
Go Vibrational Energy = ((3*Atomicity)-6)*([BoltZ]*Temperature)
Vibrational Energy of Linear Molecule
Go Vibrational Energy = ((3*Atomicity)-5)*([BoltZ]*Temperature)
Heat Capacity given Specific Heat Capacity
Go Heat Capacity = Specific Heat Capacity*Mass
Number of Modes in Non-Linear Molecule
Go Number of Normal modes for Non Linear = (6*Atomicity)-6
Vibrational Mode of Non-Linear Molecule
Go Number of Normal modes = (3*Atomicity)-6
Vibrational Mode of Linear Molecule
Go Number of Normal modes = (3*Atomicity)-5
Number of Modes in Linear Molecule
Go Number of Modes = (6*Atomicity)-5

Specific Heat Capacity given heat capacity Formula

Specific Heat Capacity = Heat Capacity/(Mass*Change in Temperature)
c = C/(Massflight path*∆T)

What is the statement of Equipartition Theorem?

The original concept of equipartition was that the total kinetic energy of a system is shared equally among all of its independent parts, on the average, once the system has reached thermal equilibrium. Equipartition also makes quantitative predictions for these energies. The key point is that the kinetic energy is quadratic in the velocity. The equipartition theorem shows that in thermal equilibrium, any degree of freedom (such as a component of the position or velocity of a particle) which appears only quadratically in the energy has an average energy of ​1⁄2kBT and therefore contributes ​1⁄2kB to the system's heat capacity.

How to Calculate Specific Heat Capacity given heat capacity?

Specific Heat Capacity given heat capacity calculator uses Specific Heat Capacity = Heat Capacity/(Mass*Change in Temperature) to calculate the Specific Heat Capacity, The Specific Heat Capacity given heat capacity of a substance is the amount of energy that must be added, in the form of heat, to one unit of mass of the substance in order to cause an increase of one unit in temperature. Specific Heat Capacity is denoted by c symbol.

How to calculate Specific Heat Capacity given heat capacity using this online calculator? To use this online calculator for Specific Heat Capacity given heat capacity, enter Heat Capacity (C), Mass (Massflight path) & Change in Temperature (∆T) and hit the calculate button. Here is how the Specific Heat Capacity given heat capacity calculation can be explained with given input values -> 2.8E-7 = 500/(35.45*50).

FAQ

What is Specific Heat Capacity given heat capacity?
The Specific Heat Capacity given heat capacity of a substance is the amount of energy that must be added, in the form of heat, to one unit of mass of the substance in order to cause an increase of one unit in temperature and is represented as c = C/(Massflight path*∆T) or Specific Heat Capacity = Heat Capacity/(Mass*Change in Temperature). The Heat Capacity is a physical property of matter, defined as the amount of heat to be supplied to a given mass of a material to produce a unit change in its temperature, Mass is the quantity of matter in a body regardless of its volume or of any forces acting on it & The Change in Temperature is the difference between the initial and final temperature.
How to calculate Specific Heat Capacity given heat capacity?
The Specific Heat Capacity given heat capacity of a substance is the amount of energy that must be added, in the form of heat, to one unit of mass of the substance in order to cause an increase of one unit in temperature is calculated using Specific Heat Capacity = Heat Capacity/(Mass*Change in Temperature). To calculate Specific Heat Capacity given heat capacity, you need Heat Capacity (C), Mass (Massflight path) & Change in Temperature (∆T). With our tool, you need to enter the respective value for Heat Capacity, Mass & Change in Temperature and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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