Optimization of the Contact Geometry between Turbine Blades and Underplatform Dampers with respect to Friction Damping

L.: Panning, Walter Sextro, K.: Popp

Publikation: Beitrag in Buch/Bericht/KonferenzbandBeitrag in einem KonferenzbandForschungBegutachtung

Originalspracheenglisch
TitelInternational Gas Turbine & Aeroengine Congress & Exhibition
Herausgeber (Verlag).
Seiten1-10
PublikationsstatusVeröffentlicht - 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/KonferenzbandBeitrag in einem KonferenzbandForschungBegutachtung

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
Panning, L.: ; Sextro, Walter ; Popp, K.:. / Optimization of the Contact Geometry between Turbine Blades and Underplatform Dampers with respect to Friction Damping. International Gas Turbine & Aeroengine Congress & Exhibition. ., 2002. S. 1-10
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