Extensions to Maskell's theory for blockage effects on bluff bodies in a closed wind tunnel

Aeronautical Journal

Volumn 105, Issue 1041-1050, 2001, Pages 409-418

  Hackett, J E ^a   Cooper, K R ^b  

^a LOCKHEED MARTIN   (United States)

^b NATIONAL RESEARCH COUNCIL CANADA   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0142081562     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/s0001924000012380     Document Type: Article

References (12)

1. MASKELL, E.G. A theory of blockage effects on bluff bodies and stalled wings in a closed wind tunnel, ARC R&M 3400, November 1963.
2. HACKETT, J.E. Tunnel-induced gradients and their effect on drag. Lockheed Engineering Report LG83ER0108, June 1983 (Revision, September 1994 is available from the author).
3. HACKETT, J.E. Drag, lift and pitching moment increments due to wall constraint in a two-dimensional wind tunnel, AIAA 38th Aerospace sciences meeting, Reno, Nevada, January 2000, paper 2000-0672.
4. HACKETT, J.E. Tunnel-induced gradients and their effect on drag, AIAA J, December 1996, 34, (12), pp 2575-2581.
5. COOPER, K.R. Comment on Tunnel-induced gradients and their effect on drag, AIAA J, 36, (2), pp 299-300.
6. HACKETT, J.E. Reply by Author to K.R. Cooper, (see Ref. 5).
7. COOPER, K.R. Improved blockage corrections for bluff bodies in closed and open wind tunnels, 10th International Conference on Wind Effects on Buildings and Structures, Sweden, June 1999.
8. COOPER, K.R. CORBER, A., STACKHOUSE, R., MOKRY, M. and HACKETT, J.E. An examination of wall-pressure-based boundary correction methods with off-centre models in a closed wind tunnel. National Research Council of Canada LTR-A-050, April 2001.
9. HACKETT, J.E. COOPER, K.R. and PERRY, M.L. Drag, lift and pitching moment increments due to wind tunnel wall constraint: extension to three dimensions. 22nd International Congress of Aeronautical Sciences, Harrogate, UK, August 2000, paper 3.7.5.
10. MOKRY, M. Automation of wall-interference procedures using the C++ object-oriented approach. AIAA 38th Aerospace Sciences meeting, Reno, Nevada, January 2000, paper 2000-0674.
11. GARNER, H.C., ROGERS, E.W.E., ACUM, W.E.A. and MASKELL, E.C. Subsonic wind tunnel wall corrections, AGARDograph 109, Paris, France, October 1966.
12. EWALD, B. (Ed.) Wind tunnel wall corrections, AGARDograph 336, AGARD, Neuilly-sur-Seine, France, 1998.