TY  - BOOK
AU  - Trescot, Charles D.
ED  - Washington. National Aeronautics and Space Administration (NASA)
TI  - 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
PY  - 1960///
CY  - Washington
PB  - NASA 
KW  - Aircraft, Fluid mechanics
KW  - Fuselages
N1  - Bound together NASA TN D-381 to 390; Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611
ER  -