Freestream turbulence effects on the development of a rotor wake
Author:
Affiliation:
1. The Pennsylvania State University, University Park, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.7813
Reference14 articles.
1. Über den Einfluß der Machzahl und der Reynoldszhal auf die aerodynamischen Beiwerte von Verdichter-Schaufelgittern bei verschiedener Turbulenz der Strömung
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1. Advance Measurement Techniques in Turbomachines;Rotating Machinery;2020-01-08
2. Flow Measurement Techniques in Turbomachinery;Springer Handbook of Experimental Fluid Mechanics;2007
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4. 3D Structure of a Rotor Wake at Mid-span and Tip Regions;34th AIAA Fluid Dynamics Conference and Exhibit;2004-06-19
5. Characteristics of combustor diffusers;Progress in Aerospace Sciences;1995-01
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