Experimental investigation of the effects of compressive stress on the flutter of a curved panel and a flat panel at supersonic mach numbers ( NASA TN D-1386)
By: Hess, Robert W.
Contributor(s): Gibson, Frederick W.
Material type:
BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington National Aeronautics and Space Administration 1962Description: 28p.Subject(s): Supersonic numbers
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | Reference | TR009554 |
Total holds: 0
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