ESDU 70018
General principles of design in relation to fatigue.
Abstract:
ESDU 70018 outlines some general principles and procedures that are relevant to the design of aircraft components subjected to fatigue loading. The matter is presented under the following headings: l. fatigue loads including a list of the major loading sources, 2. allowable stresses, 3. detail design including notes on good and bad practice, 4. effects of manufacturing procedures with a description of both beneficial and detrimental effects.Indexed under:
- Allowable Stresses
- Clamping Pressure
- Design
- Fail-Safe Structure
- Fatigue
- Fatigue Life
- Manufacturing Processes
- Roughness
- Surface Treatments
Details:
| Data Item ESDU 70018 | |
|---|---|
| Format: |
|
| Status: |
|
| Previous Releases: |
|
| ISBN: |
|
The Data Item document you have requested is available only to subscribers.
- Subscribers login here.
- If you are not an ESDU subscriber find out how to subscribe.