A Wind-tunnel Investigation of the Development of Lift on Wings in Accelerated Longitudinal Motion

Thomas R. Turner

1956 թ. հնվ · National Advisory Committee for Aeronautics

Այս էլ․ գրքի մասին

Linearized theory is used to estimate the order of magnitude of the beneficial effects that can be obtained by shaping the body of a wing-body configuration to generate lift indirectly at supersonic speeds. The analysis applies to a class of wing-body configurations which is believed to exhibit the essential features of this type of interference; the body is cylindrical upstream of a wing which has supersonic edges and the parts of the body above and below the wing are each semicircular and of different radii. Calculations are presented for a Mach number of square root of 2 for a particular family of bodies and a sonic-edge delta wing.