This report gives the operator of the Hewlett-Packard (HP-41) handheld calculator the ability to quickly and accurately determine the power requirements of a helicopter in the preliminary design phase. These power requirements are computed for three landing gear configurations: skid, fixed wheel, and retractable wheel. By comparing the power required for each configuration, the user can determine the optimum landing gear for the design.
Computer program for preliminary helicopter design
Rechnerprogramm fuer eine vorlaeufige Hubschrauberkonstruktion
US Government Reports ; Sep ; 1-126
1983
126 Seiten
Report
Englisch
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