Experimental Investigation of Endwall and Suction Side Blowing in a Highly Loaded Compressor Stator Cascade
Author:
Affiliation:
1. Institut für Strömungsmechanik, Technische Universität Braunschweig, Bienroder Weg 3, 38106 Braunschweig, Germany
2. Rolls-Royce Germany Limited and Company KG, OE-1 Compressors and Fans, Eschenweg 11, 15827 Blankenfelde-Mahlow, Germany
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4003254/5673062/021010_1.pdf
Reference18 articles.
1. Theoretical and Experimental Investigations on Aerodynamically Highly-Loaded Compressor Bladings With Boundary Layer Control;Fottner
2. Design and Test of an Ultra-Low Solidity Flow-Controlled Compressor Stator;Kirtley
3. Active Flow Separation Control of a Stator Vane Using Embedded Injection in a Multistage Compressor Experiment;Culley;ASME J. Turbomach.
4. Verdichterprofile mit Strahlklappen für den Einsatz in aerodynamisch hoch belasteten Statorgittern;Fischer
5. Two-Dimensional RANS Simulations of the Flow Through a Compressor Cascade With Jet Flaps;Fischer;Aerosp. Sci. Technol.
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