Skip Nav Destination
Close Modal
By
Amitava Ray, S.K. Dhua, K.B. Mishra, S. Jha
Search Results for
compaction
Update search
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
NARROW
Format
Topics
Book Series
Date
Availability
1-20 of 82
Search Results for compaction
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
1
Sort by
Image
Ductile tearing on a plane of maximum normal stress at the tip of a compact...
Available to PurchasePublished: 01 January 2002
Fig. 15 Ductile tearing on a plane of maximum normal stress at the tip of a compact tension specimen. Material is O1 tool steel. Source: Ref 35
More
Image
Fracture surface at position A ( Fig. 1 ), illustrating compact oxide scale...
Available to PurchasePublished: 01 June 2019
Fig. 3 Fracture surface at position A ( Fig. 1 ), illustrating compact oxide scale region within dotted line.
More
Image
Hardness profile of treated and untreated compacted graphite iron (CGI). So...
Available to PurchasePublished: 15 January 2021
Fig. 26 Hardness profile of treated and untreated compacted graphite iron (CGI). Source: Ref 36
More
Image
Wear scar and wear debris from an untreated compacted graphite iron specime...
Available to PurchasePublished: 15 January 2021
Fig. 27 Wear scar and wear debris from an untreated compacted graphite iron specimen after 72,000 impacts. Reprinted from Ref 36 with permission from Elsevier
More
Image
Wear scar and wear debris from a 2 mm (0.08 in.) induction-hardened compact...
Available to PurchasePublished: 15 January 2021
Fig. 28 Wear scar and wear debris from a 2 mm (0.08 in.) induction-hardened compacted graphite iron specimen after 72,000 impacts. Reprinted from Ref 36 with permission from Elsevier
More
Image
Wear scar and wear debris from a 3 mm (0.12 in.) induction-hardened compact...
Available to PurchasePublished: 15 January 2021
Fig. 29 Wear scar and wear debris from a 3 mm (0.12 in.) induction-hardened compacted graphite iron specimen after 72,000 impacts. Reprinted from Ref 36 with permission from Elsevier
More
Image
Profile of wear scar on an untreated compacted graphite iron specimen after...
Available to PurchasePublished: 15 January 2021
Fig. 30 Profile of wear scar on an untreated compacted graphite iron specimen after 72,000 impacts. Source: Ref 36
More
Image
Profile of wear scar on a compacted graphite iron specimen induction harden...
Available to PurchasePublished: 15 January 2021
Fig. 31 Profile of wear scar on a compacted graphite iron specimen induction hardened to a depth of 2 mm (0.08 in.) after 72,000 impacts. Source: Ref 36
More
Image
Profile of wear scar on a compacted graphite iron specimen induction harden...
Available to PurchasePublished: 15 January 2021
Fig. 32 Profile of wear scar on a compacted graphite iron specimen induction hardened to a depth of 3 mm (0.12 in.) after 72,000 impacts. Source: Ref 36
More
Image
Ductile tearing on a plane of maximum normal stress at the tip of a compact...
Available to PurchasePublished: 15 January 2021
Fig. 16 Ductile tearing on a plane of maximum normal stress at the tip of a compact tension specimen. Material is O1 tool steel. Source: Ref 11
More
Image
TEM replica of a fracture surface of a compact-tension test specimen showin...
Available to Purchase
in Failure of Nickel-Aluminum-Bronze Hydraulic Couplings, with Comments on General Procedures for Failure Analysis
> ASM Failure Analysis Case Histories: Offshore, Shipbuilding, and Marine Equipment
Published: 01 June 2019
Fig. 14 TEM replica of a fracture surface of a compact-tension test specimen showing features identified as lamellar pearlite structure, sometimes mistaken for fatigue striations 9
More
Image
Design issues led to failure of an aluminum compact heat exchanger with fla...
Available to Purchase
in Failure Analysis of Heat Exchangers
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 15 Design issues led to failure of an aluminum compact heat exchanger with flat microchannel tube and multilouver fin. (a) Controlled-atmosphere-brazed aluminum microchannel tube-fin heat-exchanger core. (b) Good brazed fin-tube joint. (c) Nonexistent joint. (d) Severe dissolution. (e
More
Image
Published: 15 May 2022
Fig. 26 Schematic of compact-tension specimen. W , width; a , crack length; B , thickness
More
Image
ASTM E399 plane-strain compact tension test results for the fractured flang...
Available to Purchase
in Brittle Fracture of the Tension Flange of a Steel Box-Girder Bridge
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1992
Fig. 16 ASTM E399 plane-strain compact tension test results for the fractured flange. Note that the test results for two different plates, CK1 and CK2, and two specimensizes (25 and 50 mm, or 1 and 2 in., thick) fell on a common curve, with no evidence of elastic-plastic behavior to at least
More
Image
in Brittle Fracture of the Tension Flange of a Steel Box-Girder Bridge
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1992
Fig. 17 Compact tension test results for 57 mm (2 1 4 in.) thick A517 grade H, heat A4071. Note the onset of elastic-plastic behavior at approximately −30°C (−20°F).
More
Book Chapter
Microstructural Manifestations of Fractured Z-Profile Steel Wires on the Outer Layer of a Failed Locked Coil Wire Rope
Available to PurchaseSeries: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.bldgs.c9001646
EISBN: 978-1-62708-219-8
... not only effective interlocking but also a continuous working surface for withstanding in-service wear. The compact construction and fill-factor of locked coil wire ropes make them relatively impervious to the ingress of moisture and render them less vulnerable to corrosion. However, such ropes...
Abstract
Locked coil wire ropes, by virtue of their unique design and construction, have specialized applications in aerial ropeways, mine hoist installations, suspension bridge cables, and so forth. In such specialty ropes, the outer layer is constructed of Z-profile wires that provide not only effective interlocking but also a continuous working surface for withstanding in-service wear. The compact construction and fill-factor of locked coil wire ropes make them relatively impervious to the ingress of moisture and render them less vulnerable to corrosion. However, such ropes are comparatively more rigid than conventional wire ropes with fiber cores and therefore are more susceptible to the adverse effects of bending stresses. The reasons for premature in-service wire rope failures are rather complex but frequently may be attributed to inappropriate wire quality and/or abusive operating environment. In either case, a systematic investigation to diagnose precisely the genesis of failure is desirable. This article provides a microstructural insight into the causes of wire breakages on the outer layer of a 40 mm diam locked coil wire rope during service. The study reveals that the breakages of Z-profile wires on the outer rope layer were abrasion induced and accentuated by arrays of fine transverse cracks that developed on a surface martensite layer.
Image
Diagram of the stages of delamination caused by repeated impact on a cerami...
Available to PurchasePublished: 01 January 2002
Fig. 14 Diagram of the stages of delamination caused by repeated impact on a ceramic surface. Stage 1 fracturing on the surface and crushing of debris; stage 2, extrusion of pulverized debris in interstices and compaction of a fine grained film; stage 3, nucleation of cracks along the weak
More
Image
Schematic diagram of the stages of delamination caused by repeated impact o...
Available to PurchasePublished: 15 January 2021
Fig. 16 Schematic diagram of the stages of delamination caused by repeated impact on a ceramic surface. Stage 1, fracturing on the surface and crushing of debris; stage 2, extrusion of pulverized debris in interstices and compaction of a fine-grained film; stage 3, nucleation of cracks along
More
Image
Specimens employed in fatigue crack propagation studies; (a) single-edge no...
Available to PurchasePublished: 15 May 2022
Fig. 6 Specimens employed in fatigue crack propagation studies; (a) single-edge notch specimen, (b) compact-tension specimen
More
Image
Illustration of debris layer of steel/steel interface. (a) Powder debris be...
Available to PurchasePublished: 15 January 2021
Fig. 32 Illustration of debris layer of steel/steel interface. (a) Powder debris bed in a steel/steel interface. Adapted from Ref 71 . (b) Debris platelets generated from the compaction and agglomeration of thin oxide debris
More
1