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COMPUTER PROGRAM USER'S MANUAL FOR ... - CAFE Foundation

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SUMMARY<br />

A major outcome of the studies sponsored by the Advanced Concept and Mission<br />

Division, A. C. M. D. of NASA under Contract No. NAS2-5885 dated 30 January 1970<br />

as reported in CR 114289 and under Contract No. NAS2-6477 dated 6 May 1971 as<br />

reported in CR 114399 has been the development of a computer program for eval-<br />

uating propeller performance (static, flight, reverse), noise, weight, and cost for<br />

general aviation aircraft propellers as a function of the prime geometric and aero-<br />

dynamic variables. Propellers have been divided into five classifications which<br />

distinguish the complexity of general aviation propellers, i. e. , fixed versus variable<br />

pitch, deicing capability, full feathering capability, and reverse thrust capability.<br />

Parameters that may be varied independently include number of blades, blade activity<br />

factor, blade integrated design lift coefficient, and blade tipspeed. A User's Manual<br />

for the computer program was written under Contract No. NAS2-6477 and is presented<br />

herein.<br />

A brief description of the technology development is presented, and a complete<br />

listing of the computer program as well as detailed instructions and samples of input<br />

and output are included. Examples of parametric studies which can be made with the<br />

computer program are shown.<br />

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