Joachim Kurzke

How to Get Component Maps for Aircraft Gas Turbine Performance Calculations

Joachim Kurzke · Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; General · 1996 · 103 citations

Engineering, Computational Engineering, Experimental Performance +13

Fundamental Differences Between Conventional and Geared Turbofans

Joachim Kurzke · 2009 · 72 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Advanced User-Friendly Gas Turbine Performance Calculations on a Personal Computer

Joachim Kurzke · Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award · 1995 · 67 citations

Engineering, Computer Science, Mechanical Engineering +17

A New Compressor Map Scaling Procedure for Preliminary Conceptional Design of Gas Turbines

Joachim Kurzke, Claus Riegler · Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery · 2000 · 55 citations

Architecture, Computational Design, Design Optimization +12

How to Create a Performance Model of a Gas Turbine From a Limited Amount of Information

Joachim Kurzke · 2005 · 52 citations

Engineering, Mechanical Engineering, Systems Engineering +17