836. A Computerized Approach to Aircraft Loadability
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Paper
836. A Computerized Approach to Aircraft Loadability. 1970.
Abstract
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.
