Evaluation of Rapid Prototyping Technologies for Use in Wind Tunnel Model Fabrication
Author:
Affiliation:
1. Air Force Research Laboratory
2. University of Dayton Research Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1301
Reference10 articles.
1. Rapid Prototyping
2. Rapid Prototyping Technology
3. Development of a Low Cost, Rapid Prototype, Lambda Wing-Body Wind Tunnel Model
4. A Joint Computational Fluid Dynamics and Experimental Fluid Dynamics Test Program
5. Development of next generation lifetime PSP imaging systems
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