Practical applications of response surface methods in the national transonic facility

39th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2001, Pages

  Deloach, Richard ^a   Hill, Jeffrey S ^a   Tomek, William G ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; DESIGN OF EXPERIMENTS; FUNCTIONS; NASA; QUALITY ASSURANCE; REYNOLDS NUMBER; SURFACE ANALYSIS; SURFACE PROPERTIES; SURFACE TESTING; TESTING; WIND STRESS;

CRYOGENIC TEMPERATURES; HIGH REYNOLDS NUMBER; INDEPENDENT VARIABLES; NASA LANGLEY RESEARCH CENTER; RESPONSE SURFACE ANALYSIS METHODS; RESPONSE SURFACE METHOD; RESPONSE SURFACE MODELING; RESPONSE SURFACE MODELS;

WIND TUNNELS;

EID: 85088183754     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-167     Document Type: Conference Paper

References (12)

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2. Gatlin, G.M., Parker, P.A. and Owens, Jr., L.R. "Development of a Semi-Span Test Capability at the National Transonic Facility". AIAA-2001- 0759. 39th AIAA Aerospace Sciences Meeting and Exhibit. Reno, NY. Jan 2001.
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