836. A Computerized Approach to Aircraft Loadability

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Title836. A Computerized Approach to Aircraft Loadability
Publication TypeConference Paper
Paper Number0836
Year of Publication1970
AuthorsPartida, J. B.
Conference29th Annual Conference, Washington, D. C., May 4-6
Conference LocationWashington, DC
PublisherSociety of Allied Weight Engineers, Inc.
Date Published5/4/70

The purpose of presenting this paper is to furnish industry with a computerized tool toward more effective aircraft loadability. The program's ability to vary input from case to case during a single run enables the user to review many aircraft configurations within a short period of time. For example, run time of 20 cases on the IBM 360 computer is approximately two minutes. The resultant computed cases are graphically presented by a Calcomp Plotter 670/565 at a rate of four minutes per case.

Key Words01. Aircraft Loading - General
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