Effect of Leading-Edge Erosion on the Performance of Transonic Compressor Blades

In this paper, an experimental and numerical investigation of the effect of leading-edge erosion in transonic blades was performed. The measurements were carried out on a linear blade cascade in the Transonic Cascade Wind Tunnel of DLR in Cologne at two operating points with an inflow Mach number of...

תיאור מלא

מידע ביבליוגרפי

Principais autores:	Alexander Hergt, Tobias Danninger, Joachim Klinner, Sebastian Grund, Manfred Beversdorff, Christian Werner-Spatz
פורמט:	Artigo
שפה:	Inglês
יצא לאור:	MDPI AG 2024-01-01
סדרה:	International Journal of Turbomachinery, Propulsion and Power
נושאים:	eroded leading edge transonic blading performance shock losses
גישה מקוונת:	https://www.mdpi.com/2504-186X/9/1/1
תגים:	הוספת תג אין תגיות, היה/י הראשונ/ה לתייג את הרשומה!