Français
You do not have access to this resource.
The Ultimate Scientific and Technical Reference
This article is included in
Aerospace systems
This offer includes:
Knowledge Base
Updated and enriched with articles validated by our scientific committees
Services
A set of exclusive tools to complement the resources
Practical Path
Operational and didactic, to guarantee the acquisition of transversal skills
Doc & Quiz
Interactive articles with quizzes, for constructive reading
Acronyms, notations and symbols
Bibliography
Standards and norms
- Standard test method for mode I interlaminar fracture toughness of unidirectional continuous fiber reinforced composite materials, ASTM International - ASTM D5528-33 - 2013
- Standard test method for plane strain-strain fracture toughness of metallic materials, ASTM International - ASTM E399-90 - 1997
Regulations
Federal Aviation Administration 25 (FAR25) – Advisory Circular 25.571, Damage tolerance and fatigue evaluation of structure (1978).
Joint Airworthiness Requirements 25 (JAR25) – Part 1: Requirements, Part 2: Acceptable means of compliance and interpretations (for composite structures: JAR25 § 25.603 and ACJ 25.603) (1978).
The Ultimate Scientific and Technical Reference
