Comment on “tunnel-induced gradients and their effect on drag”

AIAA Journal

Volumn 36, Issue 2, 1998, Pages 298-299

  Ashill, P R ^a,b   Taylor, C R ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

^b HWA Department   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85008286149     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.7518     Document Type: Note

References (5)

1. Mokry, M., "Comment on Tunnel-Induced Gradients and Their Effect on Drag,'" AIAA Journal, Vol. 36, No. 2, 1998, p. 301.
2. Hackett, J. E., "Tunnel-Induced Gradients and Their Effect on Drag," AIAA Journal, Vol. 34, No. 12, 1996, pp. 2575-2581.
3. Garner, H. C, Rogers, E. W. E., Acum, W. E. A., and Maskell, E. C., "Subsonic Wind Tunnel Wall Corrections," AGARDograph 109, Oct. 1966, pp. 319-321.
4. Taylor, C. R., "Some Fundamental Concepts in the Theory of Wind-Tunnel Wall Constraint and Its Applications," Defence Research Agency, DRA/AS/HWA/TR96055/1, 1996.
5. Woods, L. C., The Theory of Subsonic Plane Flow, Cambridge Aeronautical Series, Cambridge Univ. Press, New York, 1961, pp. 16, 17.