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
By: Washington. National Aeronautics and Space Administration (NASA).
Contributor(s): Trescot, Charles D.
Material type:
BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington NASA 1960Description: 19p.Subject(s): Aircraft, Fluid mechanics | Fuselages
| Item type | Current location | Collection | Call number | Vol info | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA TN D-381 to 390 | Not for loan | TR15610 |
Total holds: 0
Bound together NASA TN D-381 to 390
Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611
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