1-20 of 1148 Search Results for

appearance

Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Image
Published: 30 September 2023
Figure 8.33: Surface appearance of hot rolled aluminum blanks. (Courtesy Edgar Vaughan Co., Ltd., Birmingham, England) More
Image
Published: 30 June 2023
Fig. 9.24 Filiform corrosion appearance on a coated aluminum surface. Courtesy of Novelis More
Image
Published: 30 June 2023
Fig. 12.13 Roping appearance on 6 xxx ABS More
Image
Published: 01 December 2015
Fig. 26 Effect of water vapor on the fracture surface appearance of aluminum alloy 2219-T851 fatigue tested (a) in 0.101 MPa (1 atm) dry argon and (b) in 27 Pa (0.2 torr) water vapor. Testing conditions were the same except for frequency, which was 20 Hz in (a) and 5 Hz in (b More
Image
Published: 01 October 2011
Fig. 9.9 Different appearance of ferrite and cementite (Fe 3 C) constituents of pearlite when examined by optical (light) microscope and scanning electron microscope (SEM). A polished specimen is chemically etched such that the Fe 3 C platelets stand out in relief. (a) In optical microscopy More
Image
Published: 01 October 2011
Fig. 16.3 The classic appearance of erosion-corrosion in a CF-8M pump impeller. Source: Ref 16.2 More
Image
Published: 01 November 2007
Fig. 4.1 Appearance of various types of steel grains in an optical microscope. Cm, cementite More
Image
Published: 01 December 2009
Fig. 12.4 Fatigue fracture surface appearance of a failed crankshaft, showing beach marks on the lower part. The origin of the primary fracture is indicated by the arrow. Source: Ref 1 More
Image
Published: 01 December 2015
Fig. 5 Characteristic appearance of mesa corrosion resulting from CO 2 , water, and flow. Source: InterCorr International, Inc. More
Image
Published: 01 September 2008
Fig. 9 Macrograph documenting the appearance of the as-received main landing gear lever attach pin More
Image
Published: 01 September 2008
Fig. 17 Appearance of longitudinal crack in the main landing gear linear actuating piston rod cylinder More
Image
Published: 01 September 2008
Fig. 19 SEM fractographs documenting the appearance of the fracture surface. (a) Origin location (670 μm). (b) View of box A showing fracture origin. (c) Location A (5 μm). (d) Location B (2 μm). (e) Location C (5 μm). (f) Location D (2 μm) More
Image
Published: 01 September 2008
Fig. 24 Appearance of the main landing gear lever showing the location of the primary and secondary cracks. (a) Overall view (33 mm). (b) Location of primary and secondary cracks at site of ion vapor deposit (IVD) removal (10 mm) More
Image
Published: 01 September 2008
Fig. 25 Appearance of primary crack removed from part. (a) Region of primary crack where ion vapor-deposited coating had been removed (13 mm). (b) Primary crack showing branching (2 mm). (c) Fracture surface of crack after opening (3 mm) More
Image
Published: 01 September 2008
Fig. 43 Appearance of the fracture surface of the multiple-leg aircraft-handling sling More
Image
Published: 01 September 2008
Fig. 55 Micrographs showing the appearance of the cracks and microstructure. (a) Surface cracking evident. Original magnification: 50×. (b) Surface cracking and MnS inclusions. Original magnification: 100×. (c) Extended surface crack. Original magnification: 100×. (d) Intergranular crack along More
Image
Published: 01 August 2018
Fig. 17.2 (a) Appearance of the fracture of a cast iron wedge. The region near the final extremity presents a white fracture. Most of the wedge has a gray structure. Courtesy of C.H. Lopes, BR Metals Fundições Ltda, Barra do Piraí, RJ, Brazil. (b) Schematic relationship between the cooling More
Image
Published: 01 August 2018
Fig. 17.62 Appearance of the fracture surface of an old railroad wheel, made from chilled cast iron. It is possible to clearly see the white regions (close to the tread and flange), gray regions (away from the tread, close to the central region), and the intermediate mottled region. More
Image
Published: 01 September 2008
Fig. 2 Appearance of fatigue source. Original magnification: 100× More
Image
Published: 01 January 2015
Fig. 12.14 Surface appearance of a good-quality friction stir weld in 6.35 mm (0.25 in.) thick Ti-6Al-4V. Source: Ref 12.18 More