NASA Technical Note [NASA TN D-387]: Effect of streamline contouring in the wing-fuselage juncture in combination with the supersonic area rule on a sweptback-wing--fuselage configuration of high fineness ratio - Washington. National Aeronautics and Space Administration (NASA); Trescot, Charles D. (NASA Washington, 1960)
Bound together NASA TN D-381 to 390
Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611
Keywords: Aircraft, Fluid mechanics; Fuselages