Effect of strake geometry and centerbody on the lift of swept wings

Journal of Aircraft

Volumn 39, Issue 2, 2002, Pages 377-379

  Schultz, Michael P ^a,b   Flack, Karen A ^a,c  

^a UNITED STATES NAVAL ACADEMY   (United States)

^b Ocean Engineering   (United States)

^c Mechanical Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85008266429     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2938     Document Type: Article

References (7)

1. Hebbar, S. K., Platzer, M. F., and Alkhozam, A.M., "Experimental Study of Vortex Flow Control on Double-Delta Wings Using Fillets," Journal of Aircraft, Vol. 33, No. 4, 1996, pp. 743-751.
2. Lamar, J. E., "Nonlinear Lift Control at High Speed and High Angle of Attack Using Vortex Flow Technology," Special Course on Fundamentals of Fighter Aircraft Design, AGARD-R-740, Neuilly-sur-SeineCedex, France, Oct. 1987, pp. 41-423.
3. Rao, D. M., and Campbell, J. F., "Vortical Flow Management Techniques," Progress in Aerospace Sciences, Vol. 24, No. 3, 1987, pp. 173-224.
4. Kern, S., "Vortex Flow Control Using Fillets on a Double-DeltaWing," Journal of Aircraft, Vol. 30, No. 6, 1993, pp. 818-825.
5. Ghee, T. A., Gonzalez, H. A., and Findlay, D. B., "Experimental Investigation of Vortex-Tail Interaction on a 76/40 Degree Double-DeltaWing," AIAA Paper 99-3159, June 1999.
6. Barlow, J. B., Rae, W. H., and Pope, A., Low-Speed Wind Tunnel Testing, 3rd ed., Wiley, New York, 1999, pp. 234-427.
7. Coleman, H. W., and Steele, W. G., "Engineering Application of Experimental Uncertainty Analysis," AIAA Journal, Vol. 33, No. 10, 1995, pp. 1888-1896.