Wind-Tunnel Testing of an Inertial Particle Separator Inlet Using Design of Experiments-Reference-Cited by-同舟云学术

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Wind-Tunnel Testing of an Inertial Particle Separator Inlet Using Design of Experiments

Published:2013-08-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics (AFM) Conference
language:
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Author:

Oh Se-Yoon¹,Lee Jong-Geon¹,Kim Sung-Cheol¹,Kim Sangho¹

Affiliation:

1. Agency for Defense Development

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4510

Reference12 articles.

1. 1Goldsmith, E.L. and Seddon, J. "Practical Intake Aerodynamic Design," Blackwell Scientific Publications, 1993, pp.1-71.

2. 4MontgomeryD.C.,DesignandAnalysisofExperiments,6thed.,JohnWiley&Sons,Inc.,2005,pp.373-463.

3. 5Myers, R. H. and Montgomery D. C., Response Surface Methodology: Process and Product Optimization Using Designed Experiments, 1st ed.John Wiley &Sons, Inc.,1995, pp.1-123, 208-265.

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