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Coding ratio

Relations between real and coded ratios of ammonium perchlorate fractions are given by the relations ... [Pg.515]

The molecular weights of a ribonucleotide residue and a deoxyribonucleotide residue are about the same (320 and 309, respectively). Since there is a 1 1 coding ratio between DNA and RNA, the E. coli chromosome must contain ... [Pg.138]

Merging the components of the double-exponential decay into a mean lifetime does, of course, discard useful information. An example of using multiexponential decay data is shown in Fig. 5.74, right. It shows an image that displays the colour-coded ratio of the amplitude coefficients of both lifetime components. The ampli-... [Pg.139]

Whitfield and co-workers (1964) determined the molecular weight of nearly all the enzymes of the histidine operon. Adding these weights together and allowing for the dimerism of some enzymes, they calculated that the histidine operon must code the position of 4500 amino acid residues. If the size of the operon (13,000 nucleotides) is taken into account, the code ratio (nucle-otides/amino acid) in this case is 2.9/1, in good agreement with the theoretical ratio of 3/1 for a triplet code. [Pg.90]

The comparison between measured data and simulated data are good for the imaginary part, but differences appear for the real part. The ratio between simulated data and measured data is about 0.75 for TRIFOU calculation, and 1.33 for the specialised code. Those differences for the real part of the impedance signal can be explained because of the low magnitude of real part compared to imaginary part signal. [Pg.144]

It has become quite popular to optimize the manifold design using computational fluid dynamic codes, ie, FID AP, Phoenix, Fluent, etc, which solve the full Navier-Stokes equations for Newtonian fluids. The effect of the area ratio, on the flow distribution has been studied numerically and the flow distribution was reported to improve with decreasing yiR. [Pg.497]

A numerical study of the effect of area ratio on the flow distribution in parallel flow manifolds used in a Hquid cooling module for electronic packaging demonstrate the useflilness of such a computational fluid dynamic code. The manifolds have rectangular headers and channels divided with thin baffles, as shown in Figure 12. Because the flow is laminar in small heat exchangers designed for electronic packaging or biochemical process, the inlet Reynolds numbers of 5, 50, and 250 were used for three different area ratio cases, ie, AR = 4, 8, and 16. [Pg.497]

External-pressure failure of shells can result from overstress at one extreme or n om elastic instability at the other or at some intermediate loading. The code provides the solution for most shells by using a number of charts. One chart is used for cylinders where the shell diameter-to-thickness ratio and the length-to-diameter ratio are the variables. The rest of the charts depic t curves relating the geometry of cyhnders and spheres to allowable stress by cui ves which are determined from the modulus of elasticity, tangent modulus, and yield strength at temperatures for various materials or classes of materials. The text of this subsection explains how the allowable stress is determined from the charts for cylinders, spheres, and hemispherical, ellipsoidal, torispherical, and conical heads. [Pg.1024]

The test should he eondueted on design gas at design eapaeity and speed. Under the Power Test Code, the allowable departure from the speeified operating eonditions requires that the eomhined effeets of inlet pressure, inlet temperature, and speeifie gravity of gas shall not produee more than 8% departure in the inlet gas density. Agreement should he obtained to aeeept the ratio of horsepower to volume flow at the guaranteed pressure ratio and temperature as the guarantee eriteria. Another option is to ereate a new performanee eurve at the inlet temperature and pressure predieted for the time of the field test. [Pg.324]

ASME Power Test Code, 417 ASME Pressure Vessel Code, 315, 316 ASME, standard atmospheric conditions, 21 Aspect ratio, 227 Atlas Copco, 96 Automatic control systems, 356, 357... [Pg.543]

C = ASME Unfired Pressure Vessel Code constant for a vapor as described above, C is a function of the specific heat ratio, K. The equation given earlier for determining C is expressed in tabular form in Table 2. [Pg.184]

In the current review, the term effectiveness of air distribution will be used to describe the ratio of the occupied zone area (where thermal comfort and contaminant concentration are within ranges required by standards and codes) to the total occupied zone area. This hygienic criterion allows one to judge how well the HVAC system fulfills its main task—creating thermal comfort conditions and controlling contaminants in the occupied zone. [Pg.625]

The choice of these values is arbitrary. In practice, the cooling fraction will depend not only on the combustion temperature but also on the compressor delivery temperature (i.e. the pressure ratio), the allowable metal temperature and other factors, as described in Chapter 5. But with ip assumed for the first nozzle guide vane row, together with the extra total pressure loss involved (k = 0.07 in Eq. (4.48)), the rotor inlet temperature may be determined. These assumptions were used as input to the code developed by Young [11] for cycle calculations, which considers the real gas properties. [Pg.65]

Pj = the maximum initial pressure at which the combustible atmosphere exists, psig R = the ratio of the maximum deflagration pressure to the maximum initial pressure, as described in Code Par 5-3.3.1... [Pg.506]


See other pages where Coding ratio is mentioned: [Pg.391]    [Pg.736]    [Pg.515]    [Pg.519]    [Pg.520]    [Pg.429]    [Pg.433]    [Pg.434]    [Pg.364]    [Pg.311]    [Pg.391]    [Pg.736]    [Pg.515]    [Pg.519]    [Pg.520]    [Pg.429]    [Pg.433]    [Pg.434]    [Pg.364]    [Pg.311]    [Pg.2779]    [Pg.101]    [Pg.322]    [Pg.78]    [Pg.188]    [Pg.63]    [Pg.78]    [Pg.175]    [Pg.698]    [Pg.979]    [Pg.979]    [Pg.1029]    [Pg.816]    [Pg.420]    [Pg.678]    [Pg.358]    [Pg.528]    [Pg.1098]    [Pg.75]    [Pg.82]    [Pg.107]    [Pg.342]   
See also in sourсe #XX -- [ Pg.736 ]




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