Prediction of aeroelastic instabilities in rotorcraft engine design
Prediction of aeroelastic instabilities in rotorcraft engine design
Design of modern rotorcraft engines requires that aeroelastic considerations be included for prediction of instabilities due to engines-rotors-airframe interference. Computational approaches are presented which have generality in the selection of stress analysis methods are applicable to rotorcrafts involving a large number of operation variables. An instability criterion for the prediction of fatigue effects of alternating stresses on engine structural integrity is identified and applied to the corresponding airframe behavior during high speed forward flight and severe rotorcraft maneuvers. (Peters)
Dokumentinformationen
Prediction of aeroelastic instabilities in rotorcraft engine design
Vorhersage der aeroelastischen Instabilitaeten fuer die Konstruktion von Hubschraubertriebwerken
1979
29 Seiten, 66 Bilder, 48 Quellen
Aufsatz (Konferenz)
Englisch
Ähnliche Titel
Rotorcraft aeroelastic stability
| NTRS | 1988
Rotorcraft Aeroelastic Stability
| NTIS | 1988
Aeroelastic Analysis for Rotorcraft
| NTRS | 1982
Rotorcraft aeroelastic stability using robust analysis
| Online Contents | 2013
Rotorcraft Technology for HALE Aeroelastic Analysis
| NTRS | 2008