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
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
/ Charles D. Trescot
.- Washington: NASA , 1960
.- 19p .
.- ( National Aeronautics and Space Administration NASA Technical Note
Bound together NASA TN D-381 to 390 Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611
Subject Headings:
Aircraft, Fluid mechanics;
Fuselages;
Author Added Entry:
Trescot, Charles D.;
Copy Details:
Acc. No.: TR15610, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN D-381 to 390
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Bound together NASA TN D-381 to 390 Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611
Subject Headings:
Aircraft, Fluid mechanics;
Fuselages;
Author Added Entry:
Trescot, Charles D.;
Copy Details:
Acc. No.: TR15610, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN D-381 to 390
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