A PC Based Conceptual Design Package for Composite Bolted Joints AdTech Systems Research, Incorporated

Format:

Conference/Event

Author/Creator:

Rastogi, Naveen, author.

Conference Name:

World Aviation Congress & Exposition (1997-10-13 : Anaheim, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1997

Summary:

A user friendly Windows based software package is developed for analysis and design of single lap and double lap bolted joints. The bolted joint design software is based on the computer codes developed by the Northrop Corporation under a contract from the Wright Laboratory, Wright-Patterson Air Force Base, OH. Due to the low analysis time requirements, the software package is an efficient tool for use in design and optimization cycle of bolted joints involving composite materials. This work is conducted as part of a larger effort currently underway at the AdTech Systems Research, Incorporated to establish a baseline to extend the joint design methodology for generalized composite systems including life prediction, thermal effects and dissimilar materials

Notes:

Vendor supplied data

Publisher Number:

975534

Access Restriction:

Restricted for use by site license