Aeroelastic CFD Analysis of a Rotating Propeller

摘要

A new capability to conduct aeroelastic row simulations coupled withrn6 degrees of freedom motion has been added to the EZNSS row solver.rnThe new capabilities have been tested by simulating the row about anrnelastic rotating propeller under low subsonic row conditions. The resultsrnshow that elasticity does have an eu000bect on the thrust. In the currentrncase the thrust is reduced.