Effect of Rapid-Prototyped Airfoil Finish on Loading at Low Reynolds Numbers
Author:
Affiliation:
1. Aerospace and Mechanical Engineering Department, Embry-Riddle Aeronautical University, Prescott, Arizona 86301
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031811
Reference6 articles.
1. Evaluating Aerodynamic Characteristics of Wind-Tunnel Models Produced by Rapid Prototyping Methods
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3. Evaluation of Rapid Prototyping Technologies for Use in Wind Tunnel Model Fabrication
4. JacobsP. F., Stereolithography and Other RP&M Technologies, 1st ed., American Society of Mechanical Engineers, New York, 1996, pp. 1–392.
5. Influence of Layer Thickness on the Design of Rapid-Prototyped Models
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