Rotor wake characteristics of a transonic axial-flow fan
Author:
Affiliation:
1. U.S. Army Propulsion Directorate (AVSCOM), Cleveland, Ohio
2. Massachusetts Institute of Technology, Cambridge, Massachusetts
3. NASA Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9527
Reference23 articles.
1. Holographic Measurements and Theoretical Predictions of the Unsteady Flow in a Transonic Annular Cascade
2. V. Karman Vortices and their Frequency Determination in the Wakes of Profiles in the Sub- and Transonic Regimes
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