A cross influence between the blade pitch angle and the servo blade flapping angle is studied. A full mechanical equations of a rigid body motion was taken as a basis for a description of the flapping motion process. It was found that the dimensionless variables in the equations can be divided into groups by their decimal orders. The equations were truncated up to the second order of approximation error.
Язык оригиналаанглийский
Название основной публикацииProceedings of the 6th European Conference for Aerospace Sciences
СостояниеОпубликовано - 2015
Опубликовано для внешнего пользованияДа

ID: 4749617