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Fatigue design procedures : proceedings of the 4th symposium of the International Committee on Aeronautical Fatigue, held in Munich, 16-18 June 1965 /
Fatigue Design Procedures presents the full text of the papers presented at the 4th Symposium of the International Committee on Aeronautical Fatigue held in Munich, Germany on June 16-18, 1965, and summaries of the discussion held about them. The papers featured in the volume covers different aspect...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores Corporativos: | , |
| Otros Autores: | , |
| Formato: | Electrónico Congresos, conferencias eBook |
| Idioma: | Inglés |
| Publicado: |
Oxford :
Pergamon Press,
[1969]
|
| Edición: | First edition]. |
| Colección: | International series of monographs in aeronautics and astronautics. Division IX: Symposia, v. 20
|
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 111 | 2 | |a ICAF Symposium |n (4th : |d 1965 : |c Munich, Germany) | |
| 245 | 1 | 0 | |a Fatigue design procedures : |b proceedings of the 4th symposium of the International Committee on Aeronautical Fatigue, held in Munich, 16-18 June 1965 / |c edited by E. Gassner and W. Sch�utz. |
| 250 | |a First edition]. | ||
| 264 | 1 | |a Oxford : |b Pergamon Press, |c [1969] | |
| 300 | |a 1 online resource (xiii, 520 pages) : |b illustrations | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 0 | |a International series of monographs in aeronautics and astronautics. Division IX: Symposia, v. 20 | |
| 500 | |a Proceedings of the 4th of a series of meetings; proceedings of the 3d are entered under Symposium on Current Aeronautical Fatigue Problems, Rome, 1963; proceedings of the 5th are entered under Symposium on Aircraft Fatigue--Design, Operational, and Economic Aspects, Melbourne, 1967. | ||
| 504 | |a Includes bibliographical references. | ||
| 588 | 0 | |a Print version record. | |
| 505 | 0 | |a Front Cover; Fatigue Design Procedures; Copyright Page; Table of Contents; Preface; Session Chairmen; German Organizing Committee; Introduction; CHAPTER 1. FATIGUE AND FAIL-SAFE DESIGN OF A NEW JET TRANSPORT AIRPLANE; INTRODUCTION; FATIGUE AND FAIL-SAFE PHILOSOPHY; STRUCTURAL FATIGUE AND FAIL-SAFE DESIGN CRITERIA; MANUFACTURING AND METALLURGICAL DETAILS; FATIGUE ANALYSIS OF TYPICAL STRUCTURE; FULL-SCALE TESTING; SUMMARY; REFERENCES; DISCUSSION; CHAPTER 2. FAA FATIGUE STRENGTH CRITERIA AND PRACTICES; AUTHORITY FOR REQUIREMENTS; ORIGIN OF REQUIREMENTS; BASIS FOR CURRENT CRITERIA. | |
| 505 | 8 | |a Application of current fatigue requirementsmaintenance and inspection; service experience; future regulatory prospects; concluding remarks; acknowledgment; references; discussion; chapter 3. the airworthiness approach to structural fatigue; 1. introduction; 2. the general airworthiness approach; 3. fatigue, fail-safe, safe-life; 4. static and fatigue strength requirements; 5. the effect of accidents on airworthiness control; 6. accident rate-static and fatigue; 7. discussion of individual fatigue accidents and serious incidents; 8. remedial actions after accidents and incidents. | |
| 505 | 8 | |a 9. manufacturer + operator + airworthiness control = safety (approximately)10. airworthiness and the manufacturer; 11. development of full-scale fatigue testing; 12. requirements in 1965; 13. why not a quantitative statistical approach in the requirements?; 14. the usefulness of research work; 15. the future; 16. conclusion; 17. acknowledgements; references; discussion; chapter 4. the u.s. air force weapon systems fatigue certification program; a. background; b. initial fatigue certification requirements; c. the present requirements; d. program benefit summary. | |
| 505 | 8 | |a E. future areas of exploratory developmentreferences; discussion; chapter 5. trends in repeated loads on transport airplanes; introduction; general background; results and discussion; concluding remarks; references; discussion; chapter 6. material selection for service reliability; introduction; reliability; the significance of 'standard' mechanical properties in relation to fatigue behaviour; notch sensitivity and crack propagation; stress corrosion-aluminium alloy; stress corrosion and hydrogen embrittlement-high strength steels; air melted or vacuum melted steels. | |
| 505 | 8 | |a Fatigue and static strength factorsconclusions; acknowledgments; references; discussion; chapter 7. residual static strength of specimens and cracked components; 1. introduction; 2. distinction between mechanical notches and cracks; the case of a plane sheet with a centrally located notch; 3. stress intensity factor; the case of plates; 4. stability concept; study of the plates; 5. notches in bars in tension; 6. bending of semi-elliptical cracks; 7. conclusions; references; discussion; chapter 8. constant amplitude or variable amplitude tests as a basis for design studies; symbols. | |
| 520 | |a Fatigue Design Procedures presents the full text of the papers presented at the 4th Symposium of the International Committee on Aeronautical Fatigue held in Munich, Germany on June 16-18, 1965, and summaries of the discussion held about them. The papers featured in the volume covers different aspects of fatigue design. These include fail-safe design for a jet transport airplane, the weapon systems fatigue certification program of the U.S. Air Force, the role of variable amplitude or constant amplitude tests in design studies, the evaluation of allowable design stress and corresponding fatigue. | ||
| 650 | 0 | |a Airframes |x Fatigue |v Congresses. | |
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| 650 | 7 | |a TECHNOLOGY & ENGINEERING |x Engineering (General) |2 bisacsh | |
| 650 | 7 | |a Airframes |x Fatigue |2 fast |0 (OCoLC)fst00802916 | |
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| 655 | 7 | |a proceedings (reports) |2 aat |0 (CStmoGRI)aatgf300027316 | |
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| 700 | 1 | |a Gassner, E. |q (Ernst), |d 1908- |e editor. | |
| 700 | 1 | |a Sch�utz, Walter Hans, |e editor. | |
| 710 | 2 | |a International Committee on Aeronautical Fatigue. | |
| 776 | 0 | 8 | |i Print version: |t Fatigue design procedures. |b First edition] |z 0080116973 |w (DLC) 68057886 |w (OCoLC)11095 |
| 856 | 4 | 0 | |u https://sciencedirect.uam.elogim.com/science/book/9780080116976 |z Texto completo |