| Originalsprache | englisch |
|---|---|
| Titel | International Gas Turbine & Aeroengine Congress & Exhibition |
| Herausgeber (Verlag) | . |
| Seiten | 1-10 |
| Publikationsstatus | Veröffentlicht - 2002 |
Dies zitieren
Panning, L. ., Sextro, W., & Popp, K. . (2002). Optimization of the Contact Geometry between Turbine Blades and Underplatform Dampers with respect to Friction Damping. in International Gas Turbine & Aeroengine Congress & Exhibition (S. 1-10). ..
Optimization of the Contact Geometry between Turbine Blades and Underplatform Dampers with respect to Friction Damping. / Panning, L.:; Sextro, Walter; Popp, K.:.
International Gas Turbine & Aeroengine Congress & Exhibition. ., 2002. S. 1-10.Publikation: Beitrag in Buch/Bericht/Konferenzband › Beitrag in einem Konferenzband › Forschung › Begutachtung
Panning, L, Sextro, W & Popp, K 2002, Optimization of the Contact Geometry between Turbine Blades and Underplatform Dampers with respect to Friction Damping. in International Gas Turbine & Aeroengine Congress & Exhibition. ., S. 1-10.
Panning L, Sextro W, Popp K. Optimization of the Contact Geometry between Turbine Blades and Underplatform Dampers with respect to Friction Damping. in International Gas Turbine & Aeroengine Congress & Exhibition. . 2002. S. 1-10
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