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Table 4. The Parameters of Tested Surfaces of Plate AP1

in The Compensating Test System Of High Order Aspheric Plate
by Guan-Qing Lin, Mei-liang Yi

Table 1. The Parameters of Tested Surfaces of Plate P1 and P2 (c0 = 0;e2 = 0)

in The Compensating Test System Of High Order Aspheric Plate
by Guan-Qing Lin, Mei-liang Yi

Table 3. Surface Resistance of a Copper Plated Tube

in Aluminum Beam Tube For Super Collider: An Option For No-Coating No-Liner
by Chou Fermi National

Table 2: Calculation of Tank and TPS Expansions.

in Advanced Metallic Thermal Protection Systems for Reusable Launch Vehicles
by M. L. Blosser, M. L. Blosser, R. R. Chen, R. R. Chen, I. H. Schmidt, I. H. Schmidt, J. T. Dorsey, J. T. Dorsey, C. C. Poteet, C. C. Poteet, R. K. Bird, R. K. Bird 1997
"... In PAGE 11: ... The wide range of temperatures and pressures result in differences in expansion and contraction of the TPS and tank that must be accommodated to avoid damage to the TPS. To determine the expansions expected in the system, a table of load cases ( Table2 ) was created recording the temperatures and pressures at various times during the vehicle flight cycle. For each load case the temperature of the tank and the titanium inner surface of the TPS and the tank pressure are listed.... In PAGE 11: ... The displacements of the tank under a single TPS panel in the axial and hoop directions, the displacement of the inner TPS surface, and the difference between the tank and TPS . T ts co article, wh represe Fl r the ent r it te 10 American Institute of Aerona displacements are also listed in Table2 . The 15 load cases are grouped into three categories he category labeled Test Conditions represen nditions expected during testing of the integrated test ich combines the ARMOR TPS, TPSS, and a ntative tank structure.... ..."
Cited by 9

Table 1. Geometrical characteristics of test plates and of the weight Variable Symbol Units Plate A Plate B

in Fundamental Analysis Of Three-Dimensional `near Fling'
by Shigeru Sunada 1993
"... In PAGE 4: ... The configuration of the plate and the weight are shown in Fig. 2, and the dimensions of the plates and the weight are given in Table1 . The geometrical relationship between the mirror and the plate is shown in Fig.... ..."
Cited by 2

Table 1: Recognition accuracy for the tests on number plates.

in Polygonal Approximation of Closed Curves across Multiple Views
by M. Pawan Kumar, Saurabh Goyal, C. V. Jawahar, Kumar Saurabh, Goyal C. V. Jawahar, P. J. Narayanan
"... In PAGE 5: ... We are yet to test this system on a large database of number plates. Table1 shows the results ob- tained on various numerals which were obtained from num-... ..."

Table 1. Theoretical expressions of surface displacements caused by slip motion on a plate boundary.

in Slip history during one earthquake cycle at the Nankai subduction zone, inferred from the inversion analysis of levelling data with a viscoelastic slip response function
by Mitsuhiro Matsu'ura Akira, Akira Nishitani, Yukitoshi Fukahata
"... In PAGE 1: ... The method of geodetic data inversion In general, the viscoelastic surface displacements caused by slip motion along a plate bound- ary can be written in the form of hereditary integral in Eq. (1) of Table1 . Here, u indicates the total slip motion along the plate boundary , and GL is a viscoelastic slip response function.... ..."

Table 3. Aircraft Interior Surface Tests

in Evaluation of a Head Injury Criteria Component Test Device November 2004 6. Performing Organization Code 7. Author(s) 8. Performing Organization Report No.
by Richard L. Deweese, David M. Moorcroft, Deweese Rl, Moorcroft Dm 2004
"... In PAGE 11: ... For the corresponding HCTD tests, the relative position between the HCTD and the evaluation surface, as well as the accumulator pressure, was set to reproduce these critical values as closely as practical. Table3 summarizes the results of this test series. This table provides a comparison of the HCTD and sled tests, showing the head velocity, head impact angle, and the HIC and HIC duration for various aircraft interior surfaces described as follows: Polyethylene Foam Pad.... In PAGE 19: ... The ability of the HCTD to duplicate the critical parameters of impact velocity and impact angle was lim- ited by the practical constraints of velocity repeatability, impact angle adjustment increment, and the amount of laboratory time that could be spent repeating tests in an attempt to achieve the desired parameters. Therefore, some of the corresponding sled and HCTD tests shown in Table3 had differences in these critical parameters. Since HIC is directly related to impact velocity (Figure 6), it is reasonable to assume that the differences could affect the results somewhat.... ..."

Table 7: Tests for different surfaces.

in Laser Ranger Based Hazard Detection
by Lars Henriksen August, Lars Henriksen

Table 1:Angular and Positional Accuracy of Plate

in
by unknown authors
"... In PAGE 5: ... The orientation of the part was calculated from the slope of the line obtained from the image. The angular accuracy (orientation) of the test plate ranged from 0-4 degrees (see Table1 ). The positional accuracy obtained from the image analysis ranged from 0-4 mm for both X-coordinates and Y- coordinates.... ..."
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