Optimal Design of Composite-Material Panels for Business Aircraft

Format:

Conference/Event

Author/Creator:

Bert, Charles W., author.

Conference Name:

National Business Aircraft Meeting and Engineering Display (1977-03-29 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1977

Summary:

Simple design equations and optimal design procedures have been developed for determination of the optimal lamination arrangement for flat panels of filamentary composite materials under a variety of design criteria. The design criteria include buckling and material failure under uniaxial compression, fundamental frequency of free vibration and panel flutter. The equations are applied to the design of a panel typical of business aircraft and subjected to multiple design criteria

Notes:

Vendor supplied data

Publisher Number:

770453

Access Restriction:

Restricted for use by site license