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Axial points

There are a large number of variations on diis theme but each design can be defined by four parameters, namely [Pg.80]

the number of axial points (Na), usually one less than the number of points in the star design  [Pg.80]

the number of central points (Nc), usually one more than the number of replicates  [Pg.80]

In most cases, it is best to use a full factorial design for the factorial points, but if the number of factors is large, it is legitimate to reduce this and use a partial factorial design. There are almost always 2k axial points. [Pg.80]

The number of central points is often chosen according to the number of degrees of freedom required to assess errors via ANOVA and the F-test (see Sections 2.2.2 and 2.2.4.4), and should be approximately equal to the number of degrees of freedom for die lack-of-fit, with a minimum of about four unless there are special reasons for reducing diis. [Pg.80]


In dry compressors, shaft end seals are generally one of five type.s. These are labyrinth, restrictive ring, mechanical contact, liquid film, and dry gas seal. The labyrinth type is the most simple but has the highest leakage. The labyrinth seal is generally ported at an axial point between the seals in order to use an eductor or ejector to control leakage and direct it to the suction or a suitable disposal area. Alternatively, a buffer gas is used to prevent the loss of process gas. Appendix D presents a calculation method for use with labyrinth seals. [Pg.117]

With the exception of helical gears, most gear sets should not generate axial or thrust loads in normal operation. However, at least one axial (Z-axis) measurement point should be placed on each of the gear shafts. The axial point should be located at the fixed, or thrust, bearing cap and oriented toward the gearbox. [Pg.724]

Fig. 21. Comparison of time-average temperature reading from thermocouples located at different axial points on the periphery of the carbon bed for periodic flow interruption and steady-state operation. Time-average u = 1.65 mm/s for flow interruption, r = 60 min and s = 0.5. Gas and liquid inlet temperature is about 26.5°C. (Figure from Haure et al., 1989, with permission, 1989 American Institute of Chemical Engineers.)... Fig. 21. Comparison of time-average temperature reading from thermocouples located at different axial points on the periphery of the carbon bed for periodic flow interruption and steady-state operation. Time-average u = 1.65 mm/s for flow interruption, r = 60 min and s = 0.5. Gas and liquid inlet temperature is about 26.5°C. (Figure from Haure et al., 1989, with permission, 1989 American Institute of Chemical Engineers.)...
This completes the list of proper point groups, P. A summary is given in the first column of Table 2.6. All the remaining axial point groups may be generated from the proper point groups P by one or other of two methods. [Pg.39]

In this chapter, the structures and textures of carbons at different scales are explained. The carbon materials are classified into four families, diamond, graphite, fullerene, and carbyne on the basis of hybridized sp3, flat sp2, curved sp2, and sp orbitals used, respectively. Each family has its own characteristic diversity in structure and also in the possibility of accepting foreign species. The formation of these carbon materials from organic precursors (carbonization) is shortly described by dividing the process into three phases (gas, solid, and liquid), based on the intermediate phases formed during carbonization. The importance of nanotexture, mainly due to the preferred orientation of the anisotropic BSU in the graphite family, i.e., planar, axial, point, and random orientation schemes, is particularly emphasized. [Pg.73]

Steady-State Behaviour The dashed line in Figure 2 shows a typical experimental axial temperature profile for conditions listed in Table I. The banded region in the vicinity of the hot spot includes those points (labelled a, b and c) in which radial temperature profiles were also measured using moving thermocouples. There, the upper and lower lines represent the highest measured temperature and the wall temperature, respectively, at those axial points. [Pg.113]

A five-level-five-factor CCRD was employed in this study, requiring 32 experiments (Cochran and Cox, 1992). The fractional factorial design consisted of 16 factorial points, 10 axial points (two axial points on the axis of each design variable at a distance of 2 from the design center), and 6 center points. The variables and their levels selected for the study of biodiesel synthesis were reaction time (4-20 h) temperature (25-65 °C) enzyme amount (10%-50% weight of canola oil, 0.1-0.5g) substrate molar ratio (2 1—5 1 methanol canola oil) and amount of added water (0-20%, by weight of canola oil). Table 9.5 shows the independent factors (X,), levels and experimental design coded and uncoded. Thirty-two runs were performed in a totally random order. [Pg.175]

Rotatability implies that the confidence in the predictions depends only on the distance from die centre of the design. For a two factor design, this means that all experimental points hi a circle of a given radius will be predicted equally well. This has useful practical consequences, for example, if the two factors correspond to concentrations of acetone and methanol, we know that the further the concentrations are from the central point the lower is the confidence. Methods for visualising diis were described in Section 2.2.5. Rotatability does not depend on the number of replicates in the centre, but only on die value of a, which should equal j/Nj, where Nf is the number of factorial points, equal to 2k if a full factorial is used, for diis property. Note that the position of the axial points will differ if a fractional factorial is used for the cubic part of die design. [Pg.80]

Table 2.33 Position of the axial points for rotatability and orthogonality for central composite designs with varying number of replicates in the centre. Table 2.33 Position of the axial points for rotatability and orthogonality for central composite designs with varying number of replicates in the centre.
For the bulk polymerization of styrene using thermal initiation, the kinetic model of Hui and Hamielec (13) was used. The flow model (Harkness (1)) takes radial variations in temperature and concentration into account and the velocity profile was calculated at every axial point based on the radial viscosity at that point. The system equations were solved using the method of lines with a Gear routine for solving the resulting set of ordinary differential equations. [Pg.312]

Fig. 6. Distribution of experimental points in central composite designs factorial points, O centre point, x axial points... Fig. 6. Distribution of experimental points in central composite designs factorial points, O centre point, x axial points...
Fig. 4 Central composite design for three factors. The factorial points are shaded, the axial points unshaded, and the center point(s) filled. Fig. 4 Central composite design for three factors. The factorial points are shaded, the axial points unshaded, and the center point(s) filled.
If the experimental region is defined by maximum and minimum values of each factor, then the domain is cubic. The central composite design can be applied to such a situation, the axial points being set then at 1, coded values corresponding to the minimum and maximum allowed values. Other designs for the cubic domain are reviewed in Ref... [Pg.2459]

To separate the aliased square coefficients, it will be necessary to run experiments on more than two levels so that the curvatures in different directions can be discerned. This is accomplished by the experiments in the axial points. [Pg.257]


See other pages where Axial points is mentioned: [Pg.604]    [Pg.263]    [Pg.581]    [Pg.94]    [Pg.28]    [Pg.277]    [Pg.338]    [Pg.107]    [Pg.108]    [Pg.712]    [Pg.395]    [Pg.195]    [Pg.668]    [Pg.207]    [Pg.277]    [Pg.48]    [Pg.53]    [Pg.77]    [Pg.80]    [Pg.80]    [Pg.80]    [Pg.80]    [Pg.81]    [Pg.83]    [Pg.769]    [Pg.137]    [Pg.36]    [Pg.769]    [Pg.81]    [Pg.27]    [Pg.255]    [Pg.257]    [Pg.259]   
See also in sourсe #XX -- [ Pg.323 ]

See also in sourсe #XX -- [ Pg.323 ]

See also in sourсe #XX -- [ Pg.179 ]




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Point groups axial

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