Steady Performance Measurement of a Turbofan Engine with Inlet Distortions Containing Co- and Counter-Rotating Swirl from an Intake Diffuser for Hypersonic Flight
Titel Konferenzpublikation:
ASME Turbo Expo 2000: Power for Land, Sea, and Air
Untertitel Konferenzpublikation:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery Munich, Germany, May 8–11, 2000