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Author Peter Jeschke
ORIGINAL ARTICLE
Comparison of LDA and hot-wire measurements at moderate subsonic mach numbers
J. Glob. Power Propuls. Soc. 2023;7:222–241
ORIGINAL ARTICLE
Aerodynamic influence of rim seal purge flow injection on the main flow in a 1.5-stage axial turbine with nonaxisymmetric end wall contouring
J. Glob. Power Propuls. Soc. 2023;7:153–165
ORIGINAL ARTICLE
Preliminary Design of Integrated Partial Turboelectric Aircraft Propulsion Systems
Markus Pohl, Jo Köhler, Hagen Kellermann, Michael Lüdemann, Daniel Weintraub, Peter Jeschke, Mirko Hornung
J. Glob. Power Propuls. Soc. 2022;6:1–23
ORIGINAL ARTICLE
Influence of Different Gases on the Design Point of an Industrial Axial Compressor and Deduced Aerodynamical Rematching Methodology
J. Glob. Power Propuls. Soc. 2020;4:238–252
ORIGINAL ARTICLE
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
J. Glob. Power Propuls. Soc. 2019;3:639–652
ORIGINAL ARTICLE
Influence of blade geometry on secondary flow development in a transonic centrifugal compressor
J. Glob. Power Propuls. Soc. 2018;2:429–441
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