Computerized Parametric Method for Aircraft Preliminary Design Studies.
NAVAL AIR SYSTEMS COMMAND WASHINGTON DC PROFESSIONAL DEVELOPMENT CENTER
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A series of methods has been programmed which allow significant time savings in aircraft preliminary design studies. Several interesting features of these methods include Frequent application of state of the art techniques A method of calculation for wing fuel Inclusion of several geometry techniques which greatly reduce the necessity for drafting work A programmed iterative technique to choose the optimum high lift system and Application of the modular subroutine concept of programming. Author