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EBOOKCENTRAL_ocn842256549 |
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20240329122006.0 |
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060410e19960101dcu ob 000 0 eng |
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|a AU@
|b eng
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|a 9780309586603
|q (electronic bk.)
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|a 0309586607
|q (electronic bk.)
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|a AU@
|b 000050893643
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|a AU@
|b 000052938977
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|a DEBBG
|b BV044059748
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|a (OCoLC)842256549
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|b 00017961
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|a TA418.74.A33 1996
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|a 620.11223
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|a UAMI
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245 |
0 |
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|a Accelerated Aging of Materials and Structures :
|b the Effects of Long-term Elevated-temperature Exposure.
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260 |
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|a Washington :
|b National Academies Press,
|c Jan. 1996 ;
|a Ipswich :
|b Ebsco Publishing [distributor]
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300 |
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|a 1 online resource
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336 |
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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490 |
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|a Publication NMAB ;
|v 479
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504 |
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|a Includes bibliographical references.
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|a ACCELERATED AGING OF MATERIALS AND STRUCTURES; Copyright; COMMITTEE ON EVALUATION OF LONG-TERM AGING OF MATERIALS AND STRUCTURES USING ACCELERATED TEST METHODS; NATIONAL MATERIALS ADVISORY BOARD; Acknowledgments; Preface; Contents; Executive Summary; MATERIALS AGING CHARACTERIZATION; Service Environment; Materials and Degradation Mechanisms; Characterization of Aging Responses; Accelerated Methods; Analysis of Structures; REPORT ORGANIZATION; 1 Introduction; AGING OF MATERIALS AND STRUCTURES; CASE STUDY: HIGH-SPEED CIVIL TRANSPORT; 2 Aircraft Operating Environment; THE CONCORDE EXPERIENCE
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505 |
8 |
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|a HSCT CONDITIONSGround Exposure; Flight Exposure; Airframe; Engine; SUMMARY AND RECOMMENDATION; 3 Candidate Materials; ALUMINUM ALLOYS; TITANIUM ALLOYS; SUPERALLOYS; POLYMER-MATRIX COMPOSITES; Thermoset Matrices; Thermoplastic Matrices; CERAMIC-MATRIX COMPOSITES; 4 Degradation Mechanisms; ALUMINUM ALLOYS; Microstructural Changes; Residual Stresses; Strength; Toughness; Time-Dependent Deformation and Damage Accumulation; Fatigue; Creep; Environmental Effects; Summary: Aluminum Degradation Mechanisms; TITANIUM ALLOYS; Microstructural Variations; Deformation Processes; Environmental Effects
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505 |
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|a METALLIC ALLOYSThe Concorde Experience; Creep Deformation and Failure; Creep-Fatigue Failure; Creep and Creep-Fatigue Crack Growth; Acceleration and Analytical Methods; Microstructural Changes; Accelerating Creep Tests; Accelerating Fatigue Tests; POLYMER-MATRIX COMPOSITES; Current Methods; Moderate- Temperature Applications; High-Temperature Applications; Accelerated Methods; Thermal Degradation and Oxidation; Matrix Cracking; Hygrothermal Effects; CERAMIC SYSTEMS; Oxidation and Volatilization; Mechanical Response; Behavior of the Constituents; Behavior of the Composite
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|a ANALYSIS OF STRUCTURESMetallic Materials; Composite Materials; CHAPTER SUMMARY, CONCLUSIONS AND RECOMMENDATIONS; Characterization Methods; Accelerated Methods; Analysis of Structures; Approach to Materials Aging Characterization; References; Appendix Biographical Sketches of Committee Members
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520 |
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|a Titanium Degradation MechanismsSUPERALLOYS; Microstructural Changes; Deformation and Damage Accumulation; Oxidation; POLYMER-MATRIX COMPOSITES; Microstructural Changes; Damage Accumulation: Matrix Cracking; Environmental Effects; Thermal Degradation and Oxidation; Hygrothermal Effects; Summary: Polymer-Matrix Composite Degradation Mechanisms; CERAMIC-MATRIX COMPOSITES; Thermochemical Degradation; Mechanical Degradation: Effects of Corrosive Reactions; Summary: Ceramic-Matrix Composite Degradation Mechanisms; RECOMMENDATION; 5 Accelerated Methods for Characterization of Aging Response
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590 |
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
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650 |
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0 |
|a Airplanes
|x Materials
|x Deterioration.
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650 |
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0 |
|a Materials
|x Deterioration.
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650 |
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0 |
|a Metallic composites.
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650 |
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6 |
|a Avions
|x Matériaux
|x Détérioration.
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650 |
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6 |
|a Matériaux
|x Détérioration.
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650 |
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6 |
|a Composites à matrice métallique.
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650 |
|
7 |
|a Materials
|x Deterioration
|2 fast
|
650 |
|
7 |
|a Metallic composites
|2 fast
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830 |
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0 |
|a Publication NMAB ;
|v 479.
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856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=4388305
|z Texto completo
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938 |
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|a EBL - Ebook Library
|b EBLB
|n EBL4388305
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994 |
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|a 92
|b IZTAP
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