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Published: 01 January 2000
Fig. 18 Determination of the forced deflection s * for permanent deflection of 50 μm More
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Published: 01 January 1990
Fig. 23 Theoretical load-deflection diagrams for two leaf springs. In each diagram, the dashed line represents the minimum-energy spring having the same design load and ride clearance as the spring represented by the solid line. More
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Published: 01 January 2006
Fig. 5 Sequential atomic force microscopy images (contact mode, deflection image) of CP-Ti surface (etched sample, same spot). Scanning size, 5 μm; height scale, 20 nm. (a) In air. (b) Immersion in phosphate-buffered saline, 1day. (c) Two week immersion. (d) Four week immersion and after step More
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Published: 01 January 2006
Fig. 9 Wheel spider in which noncritical holes were pierced for deflection under impact and to improve bonding to plastic. Dimensions given in inches More
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Published: 01 January 2006
Fig. 5 Guide post/guide bushing deflection More
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Published: 01 January 2006
Fig. 34 Deflection contour of upper die of body-side outer subjected to static loading. Courtesy of Engineering Technology Associates, Inc. More
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Published: 09 June 2014
Fig. 21 (a) Soft area due to deflection or masking of the quench spray. (b) Microstructure of soft area More
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Published: 09 June 2014
Fig. 22 (a) Severe deflection of the quench spray caused the hardened case to visually disappear. (b) Microstructure of the case in the soft area at low magnification. (c) Microstructure of the case in the soft area at high magnification More
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Published: 01 June 2016
Fig. 9 Effect of uphill quenching on deflection of tines. Six-tine specimen was machined from 50 × 50 mm (2 × 2 in.) bar. Similar specimens machined from 25 × 25 mm (1 × 1 in.) and 75 × 75 mm (3 × 3 in.) bars had four and eight tines, respectively. More
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Published: 01 June 2016
Fig. 1 End deflection as a percentage of original thickness as cut depth increases in a 26 × 26 × 160 mm (1 × 1 × 6 in.) bar of 7010. The combined thickness of the two tines decreases. Alloy was quenched from 475 °C (890 °F) and then aged for 24 h at 120 °C (250 °F) prior to cutting. More
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Published: 01 January 1989
Fig. 21 Change in deflection versus wheel speed and down feed in the surface grinding of D6AC steel (56 HRC) Wheel grade A46K8V Cross feed, mm/pass (in./pass) 1.25 (0.050) Table speed, m/min (ft/min) 12 (40) Depth of cut, mm (in.) 0.25 (0.010) Specimen size, mm More
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Published: 01 January 1989
Fig. 22 Change in deflection versus tool wearland for the face milling of 4340 steel (quenched and tempered to 52 HRC) Tool 100 mm (4 in.) diam single-tooth face mill with Carboloy 370 (C-6) carbide End cutting edge angle 5° Peripheral clearance 8° Cutting speed, m/min (ft More
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Published: 01 January 1989
Fig. 10 Two views of the deflection of an end mill during machining showing the various components of force, F ; moment, M ; and deflection, δ. (a) Front view. (b) Side view. Source: Ref 12 More
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Published: 01 January 2005
Fig. 10 Total press deflection versus press loading obtained under dynamic loading conditions for a 500 ton Erie scotch yoke type press. Source: Ref 7 More
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Published: 01 January 2005
Fig. 14 Built-in die mismatch to compensate for ram deflection. (a) Arrangement of die impression for forging pairs of connecting rods. (b) Upper and lower dies with mismatch built into the blocker impression More
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Published: 31 October 2011
Fig. 2 Changes of deflection at the center of the lower edge of a rectangular plate due to heating by a heat source moving along the upper edge and subsequent cooling More
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Published: 31 October 2011
Fig. 9 Relationship between length of leg and curvature of longitudinal deflection in T-section beam. Source: Ref 6 , 21 More
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Published: 31 October 2011
Fig. 10 Plot of heat input versus deflection for 500 × 500 mm (20 × 20 in.) low-carbon steel panels as a function of panel thickness More
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Published: 01 January 1986
Fig. 5 Double-deflection scanning system showing a line scan with only the line coil pairs, l 1 - l 1 and l 2 - l 2 , activated. More
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Published: 01 January 1987
Fig. 31 17-4 PH stainless steel main landing-gear deflection yoke that failed because of intergranular SCC. (a) Macrograph of fracture surface. (b) Higher-magnification view of the boxed area in (a) showing area of intergranular attack. (W.L. Jensen, Lockheed Georgia Company) More