Assembly of a Passive Slat System for a CH-701 Kit Aircraft

Abstract

This report presents the background and process involved in the assembly of a passive slat system for the Zenith Air CH-701 kit aircraft. This report details the application and theory behind passive slat system. As well it lays out the tools and materials required for the job. Finally, the assembly and installation process of the slats is presented step by step. By the end of the report, the reader should have a thorough understanding of the steps involved in the assembly and installation of passive slats. Nomenclature b = wing span, ft c = wing chord, ft C Lmax = Maximum Lift Coefficient S = wing Area, ft STOL = short takeoff and landing W = weight, lbs

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Cite this paper

@inproceedings{Coenen2012AssemblyOA, title={Assembly of a Passive Slat System for a CH-701 Kit Aircraft}, author={J. Coenen and Spencer Spagnola}, year={2012} }