A Damage Tolerance Approach for Structural Integrity of Aerospace Vehicles-Reference-Cited by-同舟云学术

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A Damage Tolerance Approach for Structural Integrity of Aerospace Vehicles

Published:1985 Issue: Volume: Page:93-109
ISSN:
Container-title:Problems in Service Life Prediction of Building and Construction Materials
language:
Short-container-title:

Author:

Adams Frank D.,Engle Robert M.

Publisher

Springer Netherlands

Link

http://link.springer.com/content/pdf/10.1007/978-94-009-5125-9_6.pdf

Reference14 articles.

1. Wells, H.M., “Air Force Structural Integrity Program Requirements,” ASD-TR-66-57, Jan 1968.

2. Department of The Air Force, “Aircraft Structural Integrity Program, Airplane Requirements,” M1L-STD-1530A, Dec 1975.

3. Department of the Air Force, “Airplane Damage Tolerance Requirements,” MIL-A-83444, Jul 1974.

4. Gallagher, J.P., Gieseler, F.J., Berens, A.P. and Engle, R.M., “USAF Damage Tolerant Design Handbook: Guidelines for the Analysis and Design of Damage Tolerant Aircraft Structures,” AFWAL-TR-82-3073, Jan 1984.

5. Department of the Air Force, “Airplane Durability Design Requirements,” MIL-A-8866B, Aug 1975.

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