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In-plane design

In the x-ray portion of the spectmm, scientific CCDs have been utilized as imaging spectrometers for astronomical mapping of the sun (45), galactic diffuse x-ray background (46), and other x-ray sources. Additionally, scientific CCDs designed for x-ray detection are also used in the fields of x-ray diffraction, materials analysis, medicine, and dentistry. CCD focal planes designed for infrared photon detection have also been demonstrated in InSb (47) and HgCdTe (48) but are not available commercially. [Pg.430]

High availability and reliability are the most important parameters in the design of a gas turbine. The availability of a power plant is the percent of time the plant is available to generate power in any given period. The reliability of the plant is the percentage of time between planed overhauls. [Pg.13]

Suppose we want to analyze the stresses in the two stiffeners. The geometry of the sandwich-blade stiffener is actually more complicated and less amenable to analysis than is the hat-shaped stiffener. Issues that arise in the analysis to determine the influence of the various portions of the stiffeners include the in-plane shear stiffness. In the plane of the vertical blade is a certain amount of shear stiffness. That is, the shear stiffness is necfessary to transfer load from the 0° fibers at the top of the stiffener down to the panel. In hat-shaped stiffeners, that shear stiffness is the only way that load is transferred from the 0° fibers at the top of the stiffener down to the panel. Thus, shear stiffness is the dominant issue in the design. And that is why we typically put 45° fibers in the web of the hat-shaped stiffener. [Pg.407]

Another issue that turns out to be very important for the sandwich-blade stiffener, but not at all important for the hat-shaped stiffener, is shear in the vertical web. Not shear in the plane of the web, but shear in the plane perpendicular to the web. This transverse shear stiffness turns out to dominate the behavior or be very important in the behavior of the sandwich blade, but simply is not addressed at all in the hatshaped stiffener. You can imagine that the transverse shearing stiffness would be more important in the sandwich blade when you consider the observation that the sandwich blade is a thick element and the hatshaped stiffener is a thin element. That is, bending and in-plane shear would dominate this response, whereas transverse shear, because the sandwich blade is thick, can very easily be an important factor in the sandwich blade. For both stiffeners, appropriate analyses and design rationale have been developed to be able to make an optimally shaped stiffener. [Pg.407]

The unstiffened panel is generally designed by sizing the maximum in-plane dimensions of the panel and its minimum thickness to resist buckling. Then, the panel area dimensions can be reduced, and the thickness can be increased in the stiffened panel optimization process. [Pg.409]

Cross-sectional aiea allocated to light phase, sq ft Area of particle projected on plane normal to direction of flow or motion, sq ft Cross-sectional area at top of V essel occupied by continuous hydrocarbon phase, sq ft Actual flow at conditions, cu ft/sec Constant given in table Volume fiaction solids Overall drag coefficient, dimensionless Diameter of vessel, ft See Dp, min Cyclone diameter, ft Cyclone gas exit duct diameter, ft Hy draulic diameter, ft = 4 (flow area for phase in qiiestion/wetted perimeter) also, D in decanter design represents diameter for heavy phase, ft... [Pg.284]

From Fig. 17.1 we realize another fact. The octahedron centers are arranged in planes parallel to the a-b plane, half-way between the layers of spheres. The position of the octahedron centers corresponds to the position C which does not occur in the stacking sequence ABAB... of the spheres. We designate octahedral interstices in this position in the following sections by y. By analogy, we will designate octahedral interstices in the positions A and B by a and j3, respectively. [Pg.192]

FIGURE 26.22 Variables for calculating in-plane flow rates (transmissivity). (Adapted from U.S. EPA, Requirements for Hazardous Waste Landfill Design, Construction, and Closure, EPA/625/4-89/022, U.S. Environmental Protection Agency, Cincinnati, OH, August 1989.)... [Pg.1130]

The idea of a root locus plot is simple—if we have a computer. We pick one design parameter, say, the proportional gain Kc, and write a small program to calculate the roots of the characteristic polynomial for each chosen value of as in 0, 1, 2, 3,., 100,..., etc. The results (the values of the roots) can be tabulated or better yet, plotted on the complex plane. Even though the idea of plotting a root locus sounds so simple, it is one of the most powerful techniques in controller design and analysis when there is no time delay. [Pg.133]

As mentioned in the preceding section, Ji-effects on the stability of the reactants are going to be rather subtle in thermal cyclizations, since the determining factor in the activation barrier for this reaction is the formation of the bond between in-plane orbitals. One way to accelerate this reaction would be to destabilize the reactant ji-system. The challenge is in designing a system where the reactant destabilization is not transferred to the transition state and product as well. An elegant approach to... [Pg.22]

Tensile membrane behavior requires continuous reinforcement steel to support in-plane stesses. Two-way slabs and flat slabs, with fixed or simple supports, can usually satisfy the requirements for tensile membrane resistance. Design with tensile membrane resistance is the same as for flexural resistance since the moment capacity of the section is used to determine ultimate resistance. Tensile membrane resistance at 8 degree rotation must be at least... [Pg.103]

In addition to the in-plane loads, roof diaphragms also are subjected to normal positive overpressures and, to a less severe extent, normal negative pressures. Diaphragms should be designed to resist simultaneous in-plane and norma blast loads in conjunction with other applicable toads. The time lag between in-plane and normal loads can be taken into account in the design. The deflection of the diaphragm should be checked to confirm that it docs not exceed permissible deflections established for attached elements. [Pg.193]

This concept was proved by Kim et al. [29] using a dual-gradient CL design. Wilkinson and St-Pierre [27] presented the first use of in-plane gradienf CLs... [Pg.71]

One of the main parameters that would improve the overall performance of a fuel cell is better mass transport of reactants through the diffusion layer toward the active catalyst zones. In order to quantify and characterize how well the gas mass transport is in a specific DL material and design, it is important to measure the in-plane and through-plane permeabilities. Most of the published permeability results report the viscous permeability... [Pg.260]


See other pages where In-plane design is mentioned: [Pg.2128]    [Pg.338]    [Pg.1295]    [Pg.388]    [Pg.2128]    [Pg.338]    [Pg.1295]    [Pg.388]    [Pg.337]    [Pg.532]    [Pg.378]    [Pg.197]    [Pg.220]    [Pg.407]    [Pg.439]    [Pg.275]    [Pg.1274]    [Pg.22]    [Pg.374]    [Pg.43]    [Pg.109]    [Pg.21]    [Pg.1149]    [Pg.536]    [Pg.206]    [Pg.242]    [Pg.33]    [Pg.145]    [Pg.526]    [Pg.43]    [Pg.176]    [Pg.58]    [Pg.189]    [Pg.411]    [Pg.412]    [Pg.71]    [Pg.73]   
See also in sourсe #XX -- [ Pg.388 ]




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