K. Lehmann

Uncertainty Propagation Analyses of Lean Burn Combustor Exit Conditions for a Robust Nozzle Cooling Design

Marius Schneider, H. Schiffer, K. Lehmann, 2020 .

Parameterised Model of 2D Combustor Exit Flow Conditions for High-Pressure Turbine Simulations

Marius Schneider, H. Schiffer, K. Lehmann, 2017 .

The Influence of Combustor Swirl on Turbine Stator Endwall Heat Transfer and Film Cooling Effectiveness in a 1.5-Stage Axial Turbine

H. Schiffer, K. Lehmann, Holger Werschnik, 2015 .

Comparison of Controlled Diffusion Airfoils With Conventional NACA 65 Airfoils Developed for Stator Blade Application in a Multistage Axial Compressor

W. Steinert, H. Rechter, K. Lehmann, 1985 .

EXPERIMENTAL INVESTIGATION OF THE INFLUENCE OF FILM COOLING HOLE DIAMETER ON THE TOTAL COOLING EFFECTIVENESS FOR CYCLONE-COOLED TURBINE BLADES

K. Lehmann, Maximilian Elfner, Katharina Stichling, 2022, Proceedings of Global Power & Propulsion Society.

Comparative Experimental Investigation of Leading Edge Cooling Concepts of Turbine Rotor Blades

H. Bauer, K. Lehmann, A. Schulz, 2018, Volume 5A: Heat Transfer.

A novel test RIG for assessing advanced rotor blade cooling concepts, measurement technique and first results [in press]

Achmed Schulz, Knut Lehmann, Hans-Jörg Bauer, 2017 .