Print Email Facebook Twitter Stability of a Chinook helicopter with multiple underslung loads Title Stability of a Chinook helicopter with multiple underslung loads Author Thijs, R.J. Contributor Pavel, M.D. (mentor) Faculty Aerospace Engineering Department ASDM Programme System Engineering and Aircraft Design Date 2016-04-26 Abstract This thesis describes the process of creating numerical derived stability analysis of an Chinook with underslung loads. A helicopter model with underslung loads is build and numerically linearized. After the linearization the eigenvalues are calculated and plotted. It was found that numerical linearization works well with a single solid body, but becomes troublesome when multiple bodies are present. To reference this document use: http://resolver.tudelft.nl/uuid:e8e291ce-e6c1-41a1-83dc-826caf779f79 Part of collection Student theses Document type master thesis Rights (c) 2016 Thijs, R.J. Files PDF Stability_of_a_Chinook_he ... _loads.pdf 5.07 MB Close viewer /islandora/object/uuid:e8e291ce-e6c1-41a1-83dc-826caf779f79/datastream/OBJ/view