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As mentioned earlier in this chapter, Dreamweaver includes a couple of twists to the standard Cut, Copy, and Paste operations. Dreamweaver s Design and Code views enable you to copy and paste both text and code. Put simply, to copy only text from Dreamweaver to another application, use the Edit Copy command in Design view; to copy both text and code, use the Edit Copy command in Code view. Within Dreamweaver itself, content copied from Design view and pasted in Code view using Edit Paste appears as plain text without any code. To insert text and code, you d need to use the Edit Paste Special command and select either of the options that include formatting: Text With Structure Plus Basic Formatting or Text With Structure Plus Full Formatting.
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Rapid Prototyping of Digital Systems by James 0.Hamblen et al. contains timing information for monitors with different resolutions and refresh rates.
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Figure 11-8: Each of the 11 standard gradients has individual control handles.
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Tip Although there is no Expand/Collapse icon displayed atop the docked Files panel when a server connection is chosen, the full-window option is still available from the Options menu: Expand Files Panel. After the panel is expanded, choose the Expand/Collapse icon to return to the condensed panel view.
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vital component of the SRB system is the metadata catalog (MCAT) that manages the attributes of the digital objects in a collection. Moore and his colleagues distinguish four types of metadata for collection attributes:
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The Template Properties dialog box, shown in Figure 28-7, lists all the editable attributes found on a single page. Selecting each property brings up the editing options for that particular attribute type (text, number, color, URL, and true/false) and the current associated value. After modifying any or all of the template properties, Dreamweaver refreshes the page and displays the attributes with their new values. FIGURE 28-7
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Gradients have been given a few notable enhancements, specifically the ability to apply opacity to a gradient stop and to edit gradients live directly on an object, as shown in Figure 1.7.
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WILLIAM E. JOHNSTON, THE NASA IPG ENGINEERING TEAM, AND THE DOE SCIENCE GRID TEAM
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One of the earliest attempts to quantify coalescence frequencies was the work of Howarth (1967). A procedure was used that is similar to the one described in Section 12-3.1.5. A steady dispersion was established at a high agitation rate. The stirrer speed was then lowered so that only coalescence occurred, at least initially. Howarth de ned a global or macroscopic coalescence frequency as the initial slope of a plot of interfacial area (related to d32 ) versus time and demonstrated that systematic experiments could be conducted to determine the effect of various system variables on coalescence rate. Since the coalescence frequency depends strongly on drop diameter, most models are based on the approach discussed below. The coalescence frequency, (d, d ), is the product of the collision frequency, (d, d ), and coalescence probability, (d, d ), as shown by eq. (12-35). A schematic diagram illustrating how models for (d, d ) are developed for owdriven collisions is given in Figure 12-20. The diagram follows the overview given by Chesters (1991). From a hydrodynamic viewpoint, two separate models are developed. The model for the external ow surrounding the drops produces the collision frequency, (d, d ), approach force, F, and contact time, tc . This model can be for laminar or turbulent ow, depending on the contacting equipment and process variables. The model for the internal ow yields the lm drainage time. This model is that for a squeezing ow, driven by F and constrained by tc of the external model. Given the dimensions of the draining lm, this is a viscous model, usually assumed to be a lubrication ow. The coalescence ef ciency is determined by comparing the time to reach critical thickness with the available contact time determined by the external ow model. The approach of Figure 12-20 allows development of a variety of models. Whereas the form of (d, d ) depends on the process ow eld, that for (d, d )
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If you want to mimic full-motion video effects in Flash with as little file overhead as possible, see 36, Creating Full-Motion Video in Flash. If you want to optimize bitmaps before you bring them into Flash, see the Fireworks and Flash tutorial by Scott Brown in 30.
[49] A. V. Semenkin, S. 0. Tverdokhlebov, V. I. Garkusha, A. V. Kochergin, G. 0. Chislov, B. V. Shumkin, A. V. Solodukhin, and L. E. Zakharenkov, Operating Envelopes of Thrusters with Anode Layer, IEPC-200 1-013, 27th International Electric Propulsion Conference, Pasadena, California, October 14-19,2001. [50] D. T. Jacobson, R. S. Jankovsky, and R. K. Rawlin, High Voltage TAL Performance, AIAA-200 1-3777, 37th Joint Propulsion Conference, Salt Lake City, Utah, July 8-1 1,2001. [51] A. E. Solodukhin, A. V. Semenkin, S. 0. Tverdohlebov, and A. V. Kochergin, Parameters of D-80 Anode Layer Thruster in One and TwoStage Operation Modes, IEPC-2001-032, 27th International Electric Propulsion Conference, Pasadena, California, October 14-1 9,200 1. [52] M. Hirakawa and Y. Arakawa, Numerical Simulation of Plasma Particle Behavior in a Hall Thruster, AIAA-96-3195, 32nd Joint Propulsion Conference, Lake Buena Vista, California, July 1-3, 1996. [53] J. P. Boeuf and L. Garrigues, Low Frequency Oscillations in a Stationary Plasma Thruster, Journal of Applied Physics, vol. 84, pp. 3541-3554, 1998. [54] E. Ahedo, One-Dimensional Plasma Structure in Hall Thrusters, AIAA98-8788, 34th Joint Propulsion Conference, Cleveland, Ohio, July 13-15, 1998. [55] I. Mikellides, I. Katz, and M. Mandell, A l-D Model of the Hall-Effect Thruster with an Exhaust Region, AIAA-2001-3505, 37th Joint Propulsion Conference, Salt Lake City, Utah, July 8-1 1,200 1. [56] S. Barral, K. Makowski, Z. Peradzynski, N. Gascon, and M. Dudeck, Wall Material Effects in Stationary Plasma Thrusters. 11. Near-Wall and In-Wall Conductivity, Phys. Plasmas, vol. 10, no. 10, pp. 4137-4152, 2003. [57] F. I. Parra, E. Ahedo, J. M. Fife, and M. Martinez-Sanchez, A TwoDimensional Hybrid Model of the Hall Thruster Discharge, Journal of Applied Physics, 023304, vol. 100,2006. [58] M. Gamero-Castano and I. Katz, Estimation of Hall Thruster Erosion Using HPHall, IEPC-2005-303, 29th International Electric Propulsion Conference, Princeton University, New Jersey, October 3 l-November 4, 2005. [59] R. R. Hofer, I. Katz, I. G. Mikellides, and M. Gamero-Castano, Heavy Particle Velocity and Electron Mobility Modeling in Hybrid-PIC Hall Thruster Simulations, AIAA-2006-4658, 42nd Joint Propulsion Conference, Sacramento, California, July 9-1 2,2006.
Each additional column you add to the Criteria Range specifies an additional AND criteria. Each additional row you add to the Criteria Range specifies an additional inclusive OR criteria. The easiest way to interpret the Criteria Range is to think of the AND criteria running horizontally across and the inclusive OR criteria running vertically down the Criteria Range. The filtering action happens when you select Advanced Filter from the Excel menu. The List Range is the range of data that you normally would be filtering if you were using an AutoFilter. In this example, the List Range happens to comprise the cells A16:K67. When you run the Advanced Filter routine, you need to first select the List Range or select a cell in the first row of the List Range. In this example, it suffices to click the cell A16 before running the Advanced Filter.
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