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Adiabatic expansion and

The air spring effect results from adiabatic expansion and compression of the air in the actuator casing, Niirnericallv, the small perturbation value for air spring stiffness in Newtons/rneter is given bv Eq, (8-107),... [Pg.785]

The adiabatic expansion and compression serve only to change the temperature of tire gas widrout heat being absorbed or evolved, i.e. iso-entropic changes. The heat changes are therefore only related to the work which is done during the isothermal stages, which is given by... [Pg.60]

It follows that the efficiency of the Carnot engine is entirely determined by the temperatures of the two isothermal processes. The Otto cycle, being a real process, does not have ideal isothermal or adiabatic expansion and contraction of the gas phase due to the finite thermal losses of the combustion chamber and resistance to the movement of the piston, and because the product gases are not at tlrermodynamic equilibrium. Furthermore the heat of combustion is mainly evolved during a short time, after the gas has been compressed by the piston. This gives rise to an additional increase in temperature which is not accompanied by a large change in volume due to the constraint applied by tire piston. The efficiency, QE, expressed as a function of the compression ratio (r) can only be assumed therefore to be an approximation to the ideal gas Carnot cycle. [Pg.61]

Another method is to measure the disappearance rate of the excited parent molecules, that is, the intensity changes of the disk-like images at various delay times (therefore, at various photolysis laser positions) along the molecular beam. This is very useful when the dissociation rate is slow and the method described above cannot be applied. This measurement requires a small molecular beam velocity distribution and a large variable distance between the crossing points of the pump and probe laser beams with the molecular beam. The small velocity distribution can be obtained through adiabatic expansion, and the available distances between the pump and probe laser beams depend on the design of the chamber. For variable distances from 0 to 10 cm in our system and AV/V = 10% molecular beam velocity distribution, dissociation rates as slow as 3 x 103 s 1 under collisionless condition can be measured. [Pg.177]

USA in 1872. Thermodynamically, the cooling version consists of an adiabatic (isentropic) compression followed by heat transfer to the surroundings, then adiabatic expansion and cooling. [Pg.143]

Fig. 3 In C0NFL03, the inlet pressure was changed at time = 300 s from 150 to 200 kN/m2. Seen here are the temperature and pressure effects of the adiabatic expansion and compression. Fig. 3 In C0NFL03, the inlet pressure was changed at time = 300 s from 150 to 200 kN/m2. Seen here are the temperature and pressure effects of the adiabatic expansion and compression.
Every gas has a definite temperature (at a particular pressure) at which m = 0. Below this temperature m is positive and above this temperature m is negative. This temperature (at a particular pressure) at which m = 0, i.e., the gas neither cooled down nor heated upon adiabatic expansion and below which Chemical Equilibrium... [Pg.30]

Figure 4.3 Reversible Camot cycle, showing steps (1) reversible isothermal expansion at th (2) reversible adiabatic expansion and cooling from th to tc (3) reversible isothermal compression at tc (4) reversible adiabatic compression and heating back to the original starting point. The total area of the Camot cycle, P dV, is the net useful work w performed in the cyclic process (see text). Figure 4.3 Reversible Camot cycle, showing steps (1) reversible isothermal expansion at th (2) reversible adiabatic expansion and cooling from th to tc (3) reversible isothermal compression at tc (4) reversible adiabatic compression and heating back to the original starting point. The total area of the Camot cycle, P dV, is the net useful work w performed in the cyclic process (see text).
In Fig. 8, step I is an isothermal expansion, step II is an adiabatic expansion, step III is an isothermal compression, and step IV is an adiabatic compression. Note that zero heat is transferred in the adiabatic expansion and compression (steps II and IV) that we have added to complete the cycle, and that the work terms in these two steps exactly cancel, being equal to TC Cv dT in the expansion and Th Cv dT in the compression. (The work in an adiabatic... [Pg.78]

Here, q = 0, giving A,S sllr = 0, and the process is reversible, so q = qrcv and <7rev = 0, giving AS = 0. Because entropy is unchanged, reversible adiabatic expansions and contractions are called isentropic. [Pg.92]

Let step 12 represent the initial reversible adiabatic expansion, and step 23 the final constant-volume heating. [Pg.78]

For gases, this derivative is positive. It applies to reversible adiabatic expansions and compressions in turbines and compressors. [Pg.662]

The graphs for enthalpy also contain lines of constant entropy to permit engineering usage for 2nd law problems such as adiabatic expansion and compression of fluids. [Pg.363]

In a modification of the foregoing procedure (0. Lummer and E. Pringsheim, 1891), the stopcock is allowed to remain open after the adiabatic expansion, and the temperatures before (Pi) and immediately after (P2) expansion are measured by a sensitive thermometer. Since the corresponding pressures P and P% are known, y can be obtained from equation (10.6) in the form... [Pg.59]

How does an initially unsaturated vapor, represented by a point Lo the right of the vapor pressure curve, reach conditions under which condensation can occur Any number of paths on the [p, T) diagram are imaginable, but two are of particular interest reversible adiabatic expansion and mixing with cooler air at a lower concentration. Both proces.ses may lead 10 the formation of an aerosol composed of small liquid droplets. The paths Followed... [Pg.250]

Figure 13. Cartoon of planar gap collapse (1) initial shock from specific volume Vo = 1/po to Vt with temperature rise Tj (2) adiabatic expansion (and cooling) of ejecta spray to a mean specific volume... Figure 13. Cartoon of planar gap collapse (1) initial shock from specific volume Vo = 1/po to Vt with temperature rise Tj (2) adiabatic expansion (and cooling) of ejecta spray to a mean specific volume...
As a further stage to ensure the removal of any small particles of dust, flue gas can be directed to a Venturi-type dust collector. At both the Met and the outlet of this type of collector, dust is covered by condensate through adiabatic expansion and collected by sprayed water that is circulated via tanks installed at the inlet and the outlet, respectively. This system is also a useful preparation for the removal of traces of sulfur dioxide by passing the gases through an absorber tower where the sulfur oxides are removed by contact with circulating water that is sprayed into the tower. [Pg.529]

In expansion, the volume increases, meaning that the box gets bigger. Equation 9.12b tells us that the kinetic energy decreases, even as the quantum numbers remain constant. This is also consistent with what we know of adiabatic expansion and the kinetic model of gases the temperature of the sample drops on expansion, and temperature is related to the kinetic energy (T2 oc E). [Pg.171]

Where they have a positive slope, water cools on adiabatic expansion and warms if adiabatically compressed, and the two regions are separated by the Joule-Thompson inversion curve. Much the same information is contained in the enthalpy-pressure diagram (Figure 8.6), where it can be seen that constant enthalpy changes in pressure lead to increases in temperature in one region and decreases in another. The effect of dissolved NaCl on the Joule-Thompson coefficient has been calculated by Wood and Spera (1984), and the effect will be similar for other electrolytes. Because the addition of most electrolytes to water results in a decrease in V and in a, fijT is smaller, and the net effect is to move the inversion curve to higher temperatures, as shown in Figure 8.5. [Pg.193]

Positron and Positronium Scattering at Low Energies, J. W. Humberston How Perfect are Complete Atomic Collision Experiments H. Kleinpoppen and H. Handy Adiabatic Expansions and nonadiabatic Effects, R. McCarroll and D. S. F. Crothers Electron Capture to the Contiuum,... [Pg.422]


See other pages where Adiabatic expansion and is mentioned: [Pg.58]    [Pg.60]    [Pg.136]    [Pg.150]    [Pg.150]    [Pg.30]    [Pg.79]    [Pg.136]    [Pg.275]    [Pg.251]    [Pg.9]    [Pg.30]    [Pg.64]    [Pg.192]   


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Adiabatic expansion

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