Skip Nav Destination
Close Modal
By
P.L. Stumpff
Search Results for
composite
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 840
Search Results for composite
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
Book Chapter
Damage Assessment in a Kevlar/Polyester Composite Component
Available to PurchaseSeries: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c9001517
EISBN: 978-1-62708-217-4
... Abstract The purpose of this investigation was to determine the cause of the ultrasonic signal attenuation noted during an inspection of a composite aircraft component. Although ultrasonics was able to identify the location of the defective areas, destructive analysis had to be utilized...
Abstract
The purpose of this investigation was to determine the cause of the ultrasonic signal attenuation noted during an inspection of a composite aircraft component. Although ultrasonics was able to identify the location of the defective areas, destructive analysis had to be utilized to determine the exact nature of the defect. The investigation describes how cross-sectioning, fractography, and chemical analysis were utilized to determine the type of defect responsible for the signal attenuation.
Image
Micrograph of the worn surface for a phenolic resin-aramid fiber composite ...
Available to PurchasePublished: 01 January 2002
Fig. 9 Micrograph of the worn surface for a phenolic resin-aramid fiber composite ( Ref 29 ) showing partial coverage of the polymer pin by transfer film
More
Image
General trends indicating effect of microstructure of a composite and the p...
Available to PurchasePublished: 01 January 2002
Fig. 10 General trends indicating effect of microstructure of a composite and the properties of fillers on adhesive wear of composites. p , applied pressure; H M , hardness of matrix. AP, P, and N refer to orientations of fibers with respect to sliding direction: AP, antiparallel; P
More
Image
Specific wear rate as a function of fiber composition in hybrid composite (...
Available to PurchasePublished: 01 January 2002
Fig. 20 Specific wear rate as a function of fiber composition in hybrid composite ( L 93 N, velocity V ) 0.5 m/s, nominal V f 0.57 with dotted curve for calculated values as per equation in Ref 59 . IROM, inverse rule of mixture; LROM, linear rule of mixture. Source: Ref 59
More
Image
Composite micrograph of a transverse section through a type 303(Se) stainle...
Available to PurchasePublished: 01 January 2002
Fig. 10 Composite micrograph of a transverse section through a type 303(Se) stainless steel eye terminal for a wire rope showing corroded crack surface and final-fracture region. 75×
More
Image
Static tensile failures in carbon-graphite composite samples. Failure was b...
Available to PurchasePublished: 01 January 2002
Fig. 25 Static tensile failures in carbon-graphite composite samples. Failure was by fastener pullout. (a) Single-lap shear specimen. (b) Double-lap shear specimen. Both 1 1 3 ×
More
Image
Fatigue failure of fasteners in single-lop shear carbon-graphite composite ...
Available to PurchasePublished: 01 January 2002
Fig. 26 Fatigue failure of fasteners in single-lop shear carbon-graphite composite joints. (a) Fastener pullout resulting from a static tensile load. (b) Fatigue failure of fasteners initiated by cocking of the fasteners. Both 1 1 3 ×
More
Image
Published: 01 January 2002
Fig. 22 Plot of fretting wear versus fiber orientation angle in a composite
More
Image
A composite micrograph showing the profile of the corrosion pit. The arrow ...
Available to Purchase
in Failure Investigation of a Structural Component of the Main Landing Gear of a Transport Aircraft
> ASM Failure Analysis Case Histories: Air and Spacecraft
Published: 01 June 2019
Fig. 8 A composite micrograph showing the profile of the corrosion pit. The arrow from the dotted line marks the depth of the pit. The second arrow in the middle marks the manganese phosphate coating.
More
Image
Composite micrograph of a transverse section through a type 303(Se) stainle...
Available to Purchase
in Stress-Corrosion Cracking of a Stainless Steel Wire-Rope Terminal
> ASM Failure Analysis Case Histories: Material Handling Equipment
Published: 01 June 2019
Fig. 1 Composite micrograph of a transverse section through a type 303(Se) stainless steel eye terminal for a wire rope showing corroded crack surface and final-fracture region. 75×
More
Image
in Fatigue Failures of Links from Grab Chains
> ASM Failure Analysis Case Histories: Material Handling Equipment
Published: 01 June 2019
Fig. 2 Composite photomicrograph showing fissures adjacent to fracture. (×50).
More
Image
Published: 15 January 2021
Fig. 30 Plot of fretting wear versus fiber orientation angle in a composite
More
Image
Composite micrograph showing the grain structure of aluminum alloy 7075-T6 ...
Available to PurchasePublished: 15 January 2021
Fig. 46 Composite micrograph showing the grain structure of aluminum alloy 7075-T6 plate. Source: Ref 8
More
Image
Composite X-ray imaging of inclusions adjacent to the internal crack that w...
Available to Purchase
in Investigation of Cracking and Erratic Behavior of the Uranium-Titanium Alloy
> ASM Failure Analysis Case Histories: Processing Errors and Defects
Published: 01 June 2019
Fig. 5 Composite X-ray imaging of inclusions adjacent to the internal crack that were identified as titanium carbides.
More
Image
Elemental and composite images of inclusion cluster identified as titanium ...
Available to Purchase
in Investigation of Cracking and Erratic Behavior of the Uranium-Titanium Alloy
> ASM Failure Analysis Case Histories: Processing Errors and Defects
Published: 01 June 2019
Fig. 6 Elemental and composite images of inclusion cluster identified as titanium carbides on left and uranium oxides on right along the fracture surface.
More
Image
Composite stereomicroscope photograph of the left-hand bolt fracture surfac...
Available to Purchase
in Metallurgical Failure Analysis of Titanium Wing Attachment Bolts
> ASM Failure Analysis Case Histories: Failure Modes and Mechanisms
Published: 01 June 2019
Fig. 3 Composite stereomicroscope photograph of the left-hand bolt fracture surface inside the nut taken under oblique lighting. The fracture origin is denoted by the arrow.
More
Image
Low-magnification composite SEM micrograph of the first reducer crack. Beac...
Available to Purchase
in Cracking in a Reducing Pipe From a Pressurized Water Reactor
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1993
Fig. 4 Low-magnification composite SEM micrograph of the first reducer crack. Beach marks and surface pitting are evident
More
Image
Composite SEM fractograph of second fracture, showing multiple initiation s...
Available to Purchase
in Cracking in a Reducing Pipe From a Pressurized Water Reactor
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1993
Fig. 5 Composite SEM fractograph of second fracture, showing multiple initiation sites and beach marks
More
Image
in Ultrasonic Nondestructive Analysis of Plastics
> Characterization and Failure Analysis of Plastics
Published: 15 May 2022
Fig. 8 Ultrasonic A-scan of a composite material
More
1