Boundary layer characteristics of the Miley airfoil at low Reynolds numbers
Author:
Affiliation:
1. University of Notre Dame, Notre Dame, Indiana
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45011
Reference8 articles.
1. AERODYNAMIC MEASUREMENTS AT LOW REYNOLDS NUMBERS
2. 4Miley, S. J. "An Analysis of the Design of Airfoil Sections for Low Reynolds Numbers," Ph.D. Dissertation,Mississippi State University, Miss. Jan. 1972.
3. The influence of free-stream disturbances on low Reynolds number airfoil experiments
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