IMPROVED LOSS MODELING FOR A 2D THROUGH-FLOW COMPRESSOR DESIGN CODE

von Lanchman, Troy J.
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Gas turbine engines ; Volume 1 of 2 (2019)

COMPUTATIONAL INLET SWIRL DISTORTION INVESTIGATION OF A HIGH-SPEED COMPRESSOR

von Wolff, Marcus J. Acton, Mitch
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Gas turbine engines (2021)