Experimental flowfield measurements of missiles with square cross sections

Lijewski, Lawrence; Zollars, G. J.; Yechout, Thomas R.; Haupt, B.

doi:10.2514/6.1982-55

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“…The generation of the side-force is mainly due to asymmetric vortex location which maximizes at a roll angle of 22.51 (Lijewski et al, 1982). At this particular roll angle, one vortex is closer to the body…”

Section: Introductionmentioning

confidence: 97%

“…The prominent feature of the flow field around a rectangular cross-section fuselage is the presence of two counterrotating vortices on its leeward side, the strength of which increases with both the pitch and roll angles (Lijewski et al, 1982;Wilcox et al, 2004). The generation of the side-force is mainly due to asymmetric vortex location which maximizes at a roll angle of 22.51 (Lijewski et al, 1982).…”

Section: Introductionmentioning

confidence: 97%

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