Design of Low Reynolds Number Airfoils with Trips
Author:
Affiliation:
1. North Carolina State University, Raleigh, North Carolina 27695
2. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3157
Reference31 articles.
1. Low-Reynolds-number airfoil design for the M.I.T. Daedalus prototype- A case study
2. Design and experimental results for a high-altitude, long-endurance airfoil
3. Low Reynolds Number Airfoil Design and Wind Tunnel Testing at Princeton University
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