National transonic facility wall pressure calibration using modern design of experiments

39th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2001, Pages

  Underwood, Pamela J ^a   Everhart, Joel L ^b   DeLoach, Richard ^b  

^a VIGYAN INC   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC TESTING; EXPERIMENT DESIGN; NASA LANGLEY RESEARCH CENTER; RESPONSE SURFACE MODELS; ROBUST APPROACHES; THEORETICAL DESIGN; WALL INTERFERENCE; WIND-TUNNEL TESTING;

AEROSPACE ENGINEERING; CALIBRATION; DESIGN OF EXPERIMENTS; EXPERIMENTS; PRODUCT DESIGN;

TUNNELS;

EID: 84897848644     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Ewald, B.F.R. (Editor). Wind Tunnel Wall Corrections AGARDograph 336. October 1998.
2. st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Denver CO. June 2000.
3. th Aerospace Sciences Meeting and Exhibit, Reno NV. Jan 2000.
4. Fuller, D. "Guide for Users of the National Transonic Facility".NASA TM 83124. July 1981.
5. th Ed. New York: Wiley.
6. Myers, R.H. and Montgomery, D.C. (1995). Response Surface Methodology. New York: Wiley.
7. Box, G.E.P. and Draper, N.R. (1987). Empirical Model-Building and Response Surfaces. New York: Wiley.
8. Box, G.E.P. and Hunter, W.G. and Hunter, J.S. (1978). Statistics for Experimenters. New York: Wiley.