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Sean Tuling's Outputs (2)

Some compressibility effects on the lee side flow structures of cruciform wing-body configurations with very low aspect ratio wings (2013)
Journal Article

A series of validated numerical simulations of a tangent ogive circular body in combination with very low aspect ratio cruciform wings at supersonic Mach numbers and angles of attack up 25 have been performed. Inspection of the flow in the cross flow... Read More about Some compressibility effects on the lee side flow structures of cruciform wing-body configurations with very low aspect ratio wings.