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Kawésqar National Park

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Kawésqar National Park ( Spanish : Parque nacional Kawésqar ), formerly Alacalufes National Reserve , is the second largest national park in Chile and one of the largest in the world with an area of 7,023,542 acres. It is located between Canal Concepción and the open Pacific Ocean , on both sides of Strait of Magellan in Chile . Its area covers parts of two out of the four provinces of Magallanes and Chilean Antártica Region : Magallanes Province and Última Esperanza Province .

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63-441: There are two types of weather within the national park: "high humidity, mild cold" and, " Isothermal tundra ", with a mean temperature of 7.2 °C (45.0 °F) and 6.5 °C (43.7 °F), respectively. Rainfall can reach up to 2,450 mm (96 in) per year. The park is composed of western archipelagos; its landscape is filled with low mountain-like islands and islets and many channels and fjords. Magellanic rainforest

126-729: A n t 1 = 100 000   Pa × ( 0.001   m 3 ) 7 5 = 10 5 × 6.31 × 10 − 5   Pa m 21 / 5 = 6.31   Pa m 21 / 5 , {\displaystyle {\begin{aligned}P_{1}V_{1}^{\gamma }&=\mathrm {constant} _{1}\\&=100\,000~{\text{Pa}}\times (0.001~{\text{m}}^{3})^{\frac {7}{5}}\\&=10^{5}\times 6.31\times 10^{-5}~{\text{Pa}}\,{\text{m}}^{21/5}\\&=6.31~{\text{Pa}}\,{\text{m}}^{21/5},\end{aligned}}} so

189-466: A n t 1 = 6.31   Pa m 21 / 5 = P × ( 0.0001   m 3 ) 7 5 , {\displaystyle {\begin{aligned}P_{2}V_{2}^{\gamma }&=\mathrm {constant} _{1}\\&=6.31~{\text{Pa}}\,{\text{m}}^{21/5}\\&=P\times (0.0001~{\text{m}}^{3})^{\frac {7}{5}},\end{aligned}}} We can now solve for

252-575: A n t 2 = 10 5   Pa × 10 − 3   m 3 300   K = 0.333   Pa m 3 K − 1 . {\displaystyle {\begin{aligned}{\frac {PV}{T}}&=\mathrm {constant} _{2}\\&={\frac {10^{5}~{\text{Pa}}\times 10^{-3}~{\text{m}}^{3}}{300~{\text{K}}}}\\&=0.333~{\text{Pa}}\,{\text{m}}^{3}{\text{K}}^{-1}.\end{aligned}}} We know

315-422: A piston compressing a gas contained within a cylinder and raising the temperature where in many practical situations heat conduction through walls can be slow compared with the compression time. This finds practical application in diesel engines which rely on the lack of heat dissipation during the compression stroke to elevate the fuel vapor temperature sufficiently to ignite it. Adiabatic compression occurs in

378-461: A constant pV product (i.e., constant T ). Consider a working gas in a cylindrical chamber 1 m high and 1 m area (so 1m volume) at 400 K in static equilibrium . The surroundings consist of air at 300 K and 1 atm pressure (designated as p surr ). The working gas is confined by a piston connected to a mechanical device that exerts a force sufficient to create a working gas pressure of 2 atm (state A ). For any change in state A that causes

441-552: A final volume V B and pressure P B . As shown in Calculation of work , the heat transferred to the gas is This result is for a reversible process, so it may be substituted in the formula for the entropy change to obtain Since an ideal gas obeys Boyle's Law , this can be rewritten, if desired, as Once obtained, these formulas can be applied to an irreversible process , such as the free expansion of an ideal gas. Such an expansion

504-419: A force decrease, the gas will expand and perform work on the surroundings. Isothermal expansion continues as long as the applied force decreases and appropriate heat is added to keep pV = 2 [atm·m ] (= 2 atm × 1 m ). The expansion is said to be internally reversible if the piston motion is sufficiently slow such that at each instant during the expansion the gas temperature and pressure is uniform and conform to

567-469: A monatomic gas, 5 for a diatomic gas or a gas of linear molecules such as carbon dioxide). For a monatomic ideal gas, γ = ⁠ 5 / 3 ⁠ , and for a diatomic gas (such as nitrogen and oxygen , the main components of air), γ = ⁠ 7 / 5 ⁠ . Note that the above formula is only applicable to classical ideal gases (that is, gases far above absolute zero temperature) and not Bose–Einstein or Fermi gases . One can also use

630-423: A mountain for example, can cause the water vapor pressure to exceed the saturation vapor pressure . Expansion and cooling beyond the saturation vapor pressure is often idealized as a pseudo-adiabatic process whereby excess vapor instantly precipitates into water droplets. The change in temperature of an air undergoing pseudo-adiabatic expansion differs from air undergoing adiabatic expansion because latent heat

693-405: A pressure decrease from 2 to 1.9 atm causes a piston rise of 0.0526 m. In comparison, a pressure decrease from 1.1 to 1 atm causes a piston rise of 0.1818 m. Isothermal processes are especially convenient for calculating changes in entropy since, in this case, the formula for the entropy change, Δ S , is simply where Q rev is the heat transferred (internally reversible) to the system and T

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756-491: A protected area in South America is a stub . You can help Misplaced Pages by expanding it . Isothermal An isothermal process is a type of thermodynamic process in which the temperature T of a system remains constant: Δ T  = 0. This typically occurs when a system is in contact with an outside thermal reservoir , and a change in the system occurs slowly enough to allow the system to be continuously adjusted to

819-430: A rise in the temperature of that mass of air. The parcel of air can only slowly dissipate the energy by conduction or radiation (heat), and to a first approximation it can be considered adiabatically isolated and the process an adiabatic process. Adiabatic expansion occurs when the pressure on an adiabatically isolated system is decreased, allowing it to expand in size, thus causing it to do work on its surroundings. When

882-449: A system's behaviour. For example, according to Laplace , when sound travels in a gas, there is no time for heat conduction in the medium, and so the propagation of sound is adiabatic. For such an adiabatic process, the modulus of elasticity ( Young's modulus ) can be expressed as E = γP , where γ is the ratio of specific heats at constant pressure and at constant volume ( γ = ⁠ C p / C v ⁠ ) and P

945-465: A transition temperature, T tr , for which the two phases are in equilibrium (for example, the normal boiling point for vaporization of a liquid at one atmosphere pressure). If the transition takes place under such equilibrium conditions, the formula above may be used to directly calculate the entropy change Another example is the reversible isothermal expansion (or compression) of an ideal gas from an initial volume V A and pressure P A to

1008-445: A very high gas pressure, which ensures immediate ignition of the injected fuel. For an adiabatic free expansion of an ideal gas , the gas is contained in an insulated container and then allowed to expand in a vacuum. Because there is no external pressure for the gas to expand against, the work done by or on the system is zero. Since this process does not involve any heat transfer or work, the first law of thermodynamics then implies that

1071-512: Is absolute temperature . This formula is valid only for a hypothetical reversible process ; that is, a process in which equilibrium is maintained at all times. A simple example is an equilibrium phase transition (such as melting or evaporation) taking place at constant temperature and pressure. For a phase transition at constant pressure, the heat transferred to the system is equal to the enthalpy of transformation , Δ H tr , thus Q  = Δ H tr . At any given pressure, there will be

1134-469: Is diabatic . Some chemical and physical processes occur too rapidly for energy to enter or leave the system as heat, allowing a convenient "adiabatic approximation". For example, the adiabatic flame temperature uses this approximation to calculate the upper limit of flame temperature by assuming combustion loses no heat to its surroundings. In meteorology , adiabatic expansion and cooling of moist air, which can be triggered by winds flowing up and over

1197-501: Is 27.9% of the heat supplied to the process (- 39.1 kJ / - 140.5 kJ). This is the maximum amount of usable mechanical work obtainable from the process at the stated conditions. The percentage of W mech is a function of pV and p surr , and approaches 100% as p surr approaches zero. To pursue the nature of isothermal expansion further, note the red line on Figure 3. The fixed value of pV causes an exponential increase in piston rise vs. pressure decrease. For example,

1260-579: Is a final temperature of 753 K, or 479 °C, or 896 °F, well above the ignition point of many fuels. This is why a high-compression engine requires fuels specially formulated to not self-ignite (which would cause engine knocking when operated under these conditions of temperature and pressure), or that a supercharger with an intercooler to provide a pressure boost but with a lower temperature rise would be advantageous. A diesel engine operates under even more extreme conditions, with compression ratios of 16:1 or more being typical, in order to provide

1323-414: Is a type of thermodynamic process that occurs without transferring heat or mass between the thermodynamic system and its environment . Unlike an isothermal process , an adiabatic process transfers energy to the surroundings only as work . As a key concept in thermodynamics , the adiabatic process supports the theory that explains the first law of thermodynamics . The opposite term to "adiabatic"

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1386-434: Is also isothermal and may have the same initial and final states as in the reversible expansion. Since entropy is a state function (that depends on an equilibrium state, not depending on a path that the system takes to reach that state), the change in entropy of the system is the same as in the reversible process and is given by the formulas above. Note that the result Q  = 0 for the free expansion can not be used in

1449-415: Is always some heat loss, as no perfect insulators exist. The mathematical equation for an ideal gas undergoing a reversible (i.e., no entropy generation) adiabatic process can be represented by the polytropic process equation P V γ = constant , {\displaystyle PV^{\gamma }={\text{constant}},} where P is pressure, V is volume, and γ

1512-408: Is an isothermal process), the expression for work becomes: In IUPAC convention, work is defined as work on a system by its surroundings. If, for example, the system is compressed, then the work is done on the system by the surrounding so the work is positive and the internal energy of the system increases. Conversely, if the system expands (i.e., system surrounding expansion, so free expansions not

1575-415: Is desired to know how the values of dP and dV relate to each other as the adiabatic process proceeds. For an ideal gas (recall ideal gas law PV = nRT ) the internal energy is given by where α is the number of degrees of freedom divided by 2, R is the universal gas constant and n is the number of moles in the system (a constant). Differentiating equation (a3) yields Equation (a4)

1638-449: Is irreversible, with Δ S > 0 , as friction or viscosity are always present to some extent. The adiabatic compression of a gas causes a rise in temperature of the gas. Adiabatic expansion against pressure, or a spring, causes a drop in temperature. In contrast, free expansion is an isothermal process for an ideal gas. Adiabatic compression occurs when the pressure of a gas is increased by work done on it by its surroundings, e.g.,

1701-400: Is more than a simple 10:1 compression ratio would indicate; this is because the gas is not only compressed, but the work done to compress the gas also increases its internal energy, which manifests itself by a rise in the gas temperature and an additional rise in pressure above what would result from a simplistic calculation of 10 times the original pressure. We can solve for the temperature of

1764-423: Is produced within the system (no friction, viscous dissipation, etc.), and the work is only pressure-volume work (denoted by P d V ). In nature, this ideal kind occurs only approximately because it demands an infinitely slow process and no sources of dissipation. The other extreme kind of work is isochoric work ( d V = 0 ), for which energy is added as work solely through friction or viscous dissipation within

1827-422: Is released by precipitation. A process without transfer of heat to or from a system, so that Q = 0 , is called adiabatic, and such a system is said to be adiabatically isolated. The simplifying assumption frequently made is that a process is adiabatic. For example, the compression of a gas within a cylinder of an engine is assumed to occur so rapidly that on the time scale of the compression process, little of

1890-424: Is the adiabatic index or heat capacity ratio defined as γ = C P C V = f + 2 f . {\displaystyle \gamma ={\frac {C_{P}}{C_{V}}}={\frac {f+2}{f}}.} Here C P is the specific heat for constant pressure, C V is the specific heat for constant volume, and f is the number of degrees of freedom (3 for

1953-502: Is the ideal gas constant . In other words, the ideal gas law pV  =  nRT applies. Therefore: holds. The family of curves generated by this equation is shown in the graph in Figure 1. Each curve is called an isotherm, meaning a curve at a same temperature T . Such graphs are termed indicator diagrams and were first used by James Watt and others to monitor the efficiency of engines. The temperature corresponding to each curve in

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2016-440: Is the absolute or thermodynamic temperature . The compression stroke in a gasoline engine can be used as an example of adiabatic compression. The model assumptions are: the uncompressed volume of the cylinder is one litre (1 L = 1000 cm = 0.001 m ); the gas within is the air consisting of molecular nitrogen and oxygen only (thus a diatomic gas with 5 degrees of freedom, and so γ = ⁠ 7 / 5 ⁠ );

2079-451: Is the dominant ecosystem of the park. There are around 24 different species of mammal in the park, and the nearby national reserve is home to numerous marine species. The Kawésqar people arrived about seven thousand years ago. They were nomadic hunter-gatherers. The park is named in their honor. This Magallanes and Antártica Chilena Region location article is a stub . You can help Misplaced Pages by expanding it . This article related to

2142-534: Is the pressure of the gas. For a closed system, one may write the first law of thermodynamics as Δ U = Q − W , where Δ U denotes the change of the system's internal energy, Q the quantity of energy added to it as heat, and W the work done by the system on its surroundings. Naturally occurring adiabatic processes are irreversible (entropy is produced). The transfer of energy as work into an adiabatically isolated system can be imagined as being of two idealized extreme kinds. In one such kind, no entropy

2205-412: Is usually the case, they occur at constant pressure. Isothermal processes are often used as a starting point in analyzing more complex, non-isothermal processes. Isothermal processes are of special interest for ideal gases. This is a consequence of Joule's second law which states that the internal energy of a fixed amount of an ideal gas depends only on its temperature. Thus, in an isothermal process

2268-494: Is zero, δQ = 0 . Then, according to the first law of thermodynamics, where dU is the change in the internal energy of the system and δW is work done by the system. Any work ( δW ) done must be done at the expense of internal energy U , since no heat δQ is being supplied from the surroundings. Pressure–volume work δW done by the system is defined as However, P does not remain constant during an adiabatic process but instead changes along with V . It

2331-476: The Earth's atmosphere when an air mass descends, for example, in a Katabatic wind , Foehn wind , or Chinook wind flowing downhill over a mountain range. When a parcel of air descends, the pressure on the parcel increases. Because of this increase in pressure, the parcel's volume decreases and its temperature increases as work is done on the parcel of air, thus increasing its internal energy, which manifests itself by

2394-514: The Sahara desert . Adiabatic expansion does not have to involve a fluid. One technique used to reach very low temperatures (thousandths and even millionths of a degree above absolute zero) is via adiabatic demagnetisation , where the change in magnetic field on a magnetic material is used to provide adiabatic expansion. Also, the contents of an expanding universe can be described (to first order) as an adiabatically expanding fluid. (See heat death of

2457-512: The ideal gas law . Figure 3 shows the p – V relationship for pV = 2 [atm·m ] for isothermal expansion from 2 atm (state A ) to 1 atm (state B ). The work done (designated W A → B {\displaystyle W_{A\to B}} ) has two components. First, expansion work against the surrounding atmosphere pressure (designated as W p Δ V ), and second, usable mechanical work (designated as W mech ). The output W mech here could be movement of

2520-430: The adiabatic constant for this example is about 6.31 Pa m . The gas is now compressed to a 0.1 L (0.0001 m ) volume, which we assume happens quickly enough that no heat enters or leaves the gas through the walls. The adiabatic constant remains the same, but with the resulting pressure unknown P 2 V 2 γ = c o n s t

2583-548: The case), then the work is negative as the system does work on the surroundings and the internal energy of the system decreases. It is also worth noting that for ideal gases, if the temperature is held constant, the internal energy of the system U also is constant, and so Δ U  = 0. Since the First Law of Thermodynamics states that Δ U  =  Q  +  W in IUPAC convention, it follows that Q  = − W for

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2646-809: The compressed gas has V  = 0.1 L and P  = 2.51 × 10  Pa , so we can solve for temperature: T = P V c o n s t a n t 2 = 2.51 × 10 6   Pa × 10 − 4   m 3 0.333   Pa m 3 K − 1 = 753   K . {\displaystyle {\begin{aligned}T&={\frac {PV}{\mathrm {constant} _{2}}}\\&={\frac {2.51\times 10^{6}~{\text{Pa}}\times 10^{-4}~{\text{m}}^{3}}{0.333~{\text{Pa}}\,{\text{m}}^{3}{\text{K}}^{-1}}}\\&=753~{\text{K}}.\end{aligned}}} That

2709-396: The compressed gas in the engine cylinder as well, using the ideal gas law, PV  =  nRT ( n is amount of gas in moles and R the gas constant for that gas). Our initial conditions being 100 kPa of pressure, 1 L volume, and 300 K of temperature, our experimental constant ( nR ) is: P V T = c o n s t

2772-469: The compression ratio of the engine is 10:1 (that is, the 1 L volume of uncompressed gas is reduced to 0.1 L by the piston); and the uncompressed gas is at approximately room temperature and pressure (a warm room temperature of ~27 °C, or 300 K, and a pressure of 1 bar = 100 kPa, i.e. typical sea-level atmospheric pressure). P 1 V 1 γ = c o n s t

2835-521: The figure increases from the lower left to the upper right. In thermodynamics, the reversible work involved when a gas changes from state A to state B is where p for gas pressure and V for gas volume. For an isothermal (constant temperature T ), reversible process , this integral equals the area under the relevant PV (pressure-volume) isotherm, and is indicated in purple in Figure 2 for an ideal gas. Again, p  =  ⁠ nRT / V ⁠ applies and with T being constant (as this

2898-612: The final pressure P 2 = P 1 ( V 1 V 2 ) γ = 100 000   Pa × 10 7 / 5 = 2.51 × 10 6   Pa {\displaystyle {\begin{aligned}P_{2}&=P_{1}\left({\frac {V_{1}}{V_{2}}}\right)^{\gamma }\\&=100\,000~{\text{Pa}}\times {\text{10}}^{7/5}\\&=2.51\times 10^{6}~{\text{Pa}}\end{aligned}}} or 25.1 bar. This pressure increase

2961-424: The formula for the entropy change since the process is not reversible. The difference between the reversible and irreversible is found in the entropy of the surroundings. In both cases, the surroundings are at a constant temperature, T , so that Δ S sur  = − ⁠ Q / T ⁠ ; the minus sign is used since the heat transferred to the surroundings is equal in magnitude and opposite in sign to

3024-400: The gas increases the internal energy and will tend to increase the temperature. To maintain the constant temperature energy must leave the system as heat and enter the environment. If the gas is ideal, the amount of energy entering the environment is equal to the work done on the gas, because internal energy does not change. For isothermal expansion, the energy supplied to the system does work on

3087-518: The heat Q transferred to the system. In the reversible case, the change in entropy of the surroundings is equal and opposite to the change in the system, so the change in entropy of the universe is zero. In the irreversible, Q  = 0, so the entropy of the surroundings does not change and the change in entropy of the universe is equal to ΔS for the system. Adiabatic process An adiabatic process ( adiabatic from Ancient Greek ἀδιάβατος ( adiábatos )  'impassable')

3150-456: The ideal gas law to rewrite the above relationship between P and V as P 1 − γ T γ = constant , T V γ − 1 = constant {\displaystyle {\begin{aligned}P^{1-\gamma }T^{\gamma }&={\text{constant}},\\TV^{\gamma -1}&={\text{constant}}\end{aligned}}} where T

3213-425: The internal energy of an ideal gas is constant. This is a result of the fact that in an ideal gas there are no intermolecular forces . Note that this is true only for ideal gases; the internal energy depends on pressure as well as on temperature for liquids, solids, and real gases. In the isothermal compression of a gas there is work done on the system to decrease the volume and increase the pressure. Doing work on

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3276-427: The isothermal compression or expansion of ideal gases. The reversible expansion of an ideal gas can be used as an example of work produced by an isothermal process. Of particular interest is the extent to which heat is converted to usable work, and the relationship between the confining force and the extent of expansion. During isothermal expansion of an ideal gas, both p and V change along an isotherm with

3339-401: The net internal energy change of the system is zero. For an ideal gas, the temperature remains constant because the internal energy only depends on temperature in that case. Since at constant temperature, the entropy is proportional to the volume, the entropy increases in this case, therefore this process is irreversible. The definition of an adiabatic process is that heat transfer to the system

3402-448: The piston used to turn a crank-arm, which would then turn a pulley capable of lifting water out of flooded salt mines . The system attains state B ( pV = 2 [atm·m ] with p = 1 atm and V = 2 m ) when the applied force reaches zero. At that point, W A → B {\displaystyle W_{A\to B}} equals –140.5 kJ, and W p Δ V is –101.3 kJ. By difference, W mech = –39.1 kJ, which

3465-475: The pressure applied on a parcel of gas is reduced, the gas in the parcel is allowed to expand; as the volume increases, the temperature falls as its internal energy decreases. Adiabatic expansion occurs in the Earth's atmosphere with orographic lifting and lee waves , and this can form pilei or lenticular clouds . Due in part to adiabatic expansion in mountainous areas, snowfall infrequently occurs in some parts of

3528-409: The process is also isothermal. Thus, specifying that a process is isothermal is not sufficient to specify a unique process. For the special case of a gas to which Boyle's law applies, the product pV ( p for gas pressure and V for gas volume) is a constant if the gas is kept at isothermal conditions. The value of the constant is nRT , where n is the number of moles of the present gas and R

3591-428: The shallower the material is in the Earth. Such temperature changes can be quantified using the ideal gas law , or the hydrostatic equation for atmospheric processes. In practice, no process is truly adiabatic. Many processes rely on a large difference in time scales of the process of interest and the rate of heat dissipation across a system boundary, and thus are approximated by using an adiabatic assumption. There

3654-456: The surroundings. In either case, with the aid of a suitable linkage the change in gas volume can perform useful mechanical work. For details of the calculations, see calculation of work . For an adiabatic process , in which no heat flows into or out of the gas because its container is well insulated, Q  = 0. If there is also no work done, i.e. a free expansion , there is no change in internal energy. For an ideal gas, this means that

3717-402: The system's energy can be transferred out as heat to the surroundings. Even though the cylinders are not insulated and are quite conductive, that process is idealized to be adiabatic. The same can be said to be true for the expansion process of such a system. The assumption of adiabatic isolation is useful and often combined with other such idealizations to calculate a good first approximation of

3780-480: The system. A stirrer that transfers energy to a viscous fluid of an adiabatically isolated system with rigid walls, without phase change, will cause a rise in temperature of the fluid, but that work is not recoverable. Isochoric work is irreversible. The second law of thermodynamics observes that a natural process, of transfer of energy as work, always consists at least of isochoric work and often both of these extreme kinds of work. Every natural process, adiabatic or not,

3843-577: The temperature of the reservoir through heat exchange (see quasi-equilibrium ). In contrast, an adiabatic process is where a system exchanges no heat with its surroundings ( Q  = 0). Simply, we can say that in an isothermal process while in adiabatic processes: The noun isotherm is derived from the Ancient Greek words ἴσος ( ísos ), meaning "equal", and θέρμη ( thérmē ), meaning "heat". Isothermal processes can occur in any kind of system that has some means of regulating

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3906-508: The temperature, including highly structured machines , and even living cells. Some parts of the cycles of some heat engines are carried out isothermally (for example, in the Carnot cycle ). In the thermodynamic analysis of chemical reactions , it is usual to first analyze what happens under isothermal conditions and then consider the effect of temperature. Phase changes , such as melting or evaporation , are also isothermal processes when, as

3969-415: The universe .) Rising magma also undergoes adiabatic expansion before eruption, particularly significant in the case of magmas that rise quickly from great depths such as kimberlites . In the Earth's convecting mantle (the asthenosphere) beneath the lithosphere , the mantle temperature is approximately an adiabat. The slight decrease in temperature with shallowing depth is due to the decrease in pressure

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