Normaly in turbomachinery , a coexistance of lateral forces from entry swirl flow and from shaft rotation has to be ... (aquot;back to backaquot;) have been- analysed in order to show the influence of the attack location (Pos.x) on the aerodynamic excitation.
|Title||:||Rotordynamic instability problems in high-performance turbomachinery|
|Author||:||United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, United States. Army Research Office, Texas A & M University, Lewis Research Center|