Results 271 to 280 of about 355,992 (315)
Some of the next articles are maybe not open access.

Evaluation of damage tolerance in aircraft structures

15th Structural Dynamics and Materials Conference, 1974
The specific requirements and the evaluation procedures used to qualify the damage tolerance of two competing wing carrythrough structure designs are reviewed. One design is principally beta-processed 6A1-4V titanium in a fail safe configuration, and the other is principally 10 Ni steel in a monolithic configuration.
H. I. McHenry, E. K. Hensley
openaire   +1 more source

Design for damage tolerance

Journal of Aircraft, 1970
The emergence of damage tolerance as a primary design consideration for new generations of aircraft is shown to be the result of concern for increased safety and reliability by airframe manufacturers and regulatory bodies. Design criteria applicable to the case of structurally damaged components are defined.
openaire   +1 more source

Contact Damage and Damage Tolerance of Dental Ceramics

Key Engineering Materials, 2006
Surface and subsurface contact damage in dental ceramics and the influence of microstructure on damage tolerance were investigated in this study through indentation methods. The dependence of the damage tolerance on common materials properties was discussed.
Yan Qiu, Yi Wang Bao, Yi Hong Liu
openaire   +1 more source

Approximations in Optimization of Damage Tolerant Structures

AIAA Journal, 2000
Approximations for structural response and design sensitivities signie cantly reduce the computational cost of structural optimization. To be useful, the approximation must be accurate and computationally efe cient. Damage tolerant design puts even more stringent computational demands on optimization procedures and approximations ...
John H. Garcelon   +2 more
openaire   +1 more source

Damage tolerance aspects

2001
The spirit of Glare is its crack bridging mechanism, which provides superior damage tolerance properties. Depending on the specific property, Glare shows either monolithic metal or composite behaviour. This challenges the definition of strength justification and certification procedures.
openaire   +1 more source

Assessment of damage tolerance in composites

Composite Structures, 1985
Abstract Damage tolerance to processing and normal service damage has been assessed for carbon epoxy coupons and built-up panels in uniaxial loading. In coupons, the low velocity impact damage is more severe than damage in holes, delaminations or porosity and it causes compression strength loss from 58% at the barely visible threshold to 73% at the ...
E. Demuts, R.S. Whitehead, R.B. Deo
openaire   +1 more source

Damage tolerance substantiation

1989
Previous chapters dealt with analysis procedures, (Chapters 2-5), the ingredients needed for the analysis (Chapters 7-10) and with the use of the results for fracture control (Chapter 11). This Chapter concentrates on the general scope of the analysis, its relationship to tests (verification and substantiation), the assumptions and sources of error ...
openaire   +1 more source

Damage Tolerance of Metals

2005
Abstract This chapter presents a fracture-mechanics-based approach to damage tolerance, accounting for mechanical, metallurgical, and environmental factors that drive crack development and growth. It begins with a review of stress-intensity factors corresponding to a wide range of crack geometries, specimen configurations, and loading ...
openaire   +1 more source

Durability and Damage Tolerance of Composites

2001
In certain structural applications the use of fiber composites is advantageous over metallic structures (lighter weight, and higher stiffness). Polymer matrix composite (PMC) materials with continuous high modulus graphite fibers are very effective under high-cycle fatigue loading due to the ability of fibers to transmit and disperse the high-frequency
Frank Abdi   +2 more
openaire   +1 more source

Damage Accumulation Techniques in Damage Tolerance Analysis

1984
Damage tolerance analysis requires the capability to assess the damage, usually measured by incremental crack growth, accumulating in a given piece of structure under flight-by-flight spectrum loading. This requirement implies the need to process this damage accumulation over thousands of flights consisting of millions of load cycles.
openaire   +1 more source

Home - About - Disclaimer - Privacy