Large Cargo Airplane Structural Considerations

Format:

Conference/Event

Author/Creator:

Shuler, W. T., author.

Conference Name:

National Aeronautic and Space Engineering and Manufacturing Meeting (1966-10-03 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1966

Summary:

This discussion summarizes the highlights of the C-141A airplane program, emphasizing fatigue, damage tolerance, and static strength considerations philosophically and in considerable detail where design criteria are involved. Dynamic considerations are also included insofar as the structural design of the airplane was affected thereby. Finally, some significant differences in criteria requirements between the C-141A and the C-5A are identified together with their expected impact on structural design

Notes:

Vendor supplied data

Publisher Number:

660669

Access Restriction:

Restricted for use by site license