Shuttle Debris Impact Tool Assessment Using the Modern Design of Experiments
Author:
Affiliation:
1. NASA Langley Research Center
2. NASA Johnson Space Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-550
Reference14 articles.
1. Applications of modern experiment design to wind tunnel testing at NASA Langley Research Center
2. Tailoring wind tunnel data volume requirements through the formal design of experiments
3. Tactical defenses against systematic variation in wind tunnel testing
4. 5Fisher,M.S.,SoftwareVerificationandValidation:AnEngineeringandScientificApproach,Springer,Cambridge,2006.
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