A numerical method for calculating the flat-plate pressure distribution on supersonic wings of supersonic wings of arbitrary planform. [NASA TN D-2570]
By: Wilbur, D. Middleton.
Contributor(s): Carlson, Harry W.
Material type:
BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D. C NASA 1965Description: 23p.Subject(s): Arbitrary
Contents:
NASA technical report
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA TN D-2570 (Browse shelf) | Not for loan | TR83084 |
Total holds: 0
NASA technical report
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