Verantwortliches Institut
Das Projekt wurde verantwortet durch das Institut für Flugantriebe und Strömungsmaschinen (TU Braunschweig).
Teilprojektleiter
Hermann-Blenk-Strasse 37
38108 Braunschweig
Hermann-Blenk-Strasse 37
38108 Braunschweig
Veröffentlichungen
Internationale wissenschaftliche Beiträge in Fachzeitschriften, begutachtet
-
(2018): Sensitivity analysis of blisk airfoil wear , International Journal of Turbomachinery, Propulsion and Power 2018, 3(2), 14
DOI: 10.3390/ijtpp3020014 -
(2018): Deterioration effects of coupled blisk blades, Journal of the Global Power and Propulsion Society. 2: 465–476.
DOI: 10.22261/JGPPS.CKB8N6
Internationale Konferenzbeiträge, begutachtet
-
(2018): Deterioration effects of coupled blisk blades, Global Power and Propulsion Forum, Proceedings of Montreal 2018
-
(2017): Influence of Geometric Imperfections on Aerodynamic and Aeroelastic Behavior of a Compressor Blisk, In: Proceedings of ASME Turbo Expo 2017, Charlotte, USA, GT2017-63556
-
(2017): Sensitivity analysis of blisk airfoil wear, ISROMAC 2017 - 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Maui, USA, Dec 16-21.
-
(2014): Numerical investigation of circumferential coupled deterioration effects of a jet engine compressor front stage compared to BLISK geometry, Proceedings of the 3rd International Conference in Through-life Engineering Services 2014 (22), S. 249–255
DOI: 10.1016/j.procir.2014.07.006
Nationale Konferenzbeiträge, nicht begutachtet
-
(2015): Performance impact of high pressure compressor blisk roughness., DLRK 2015. DGLR. Rostock, 01.01.2015.