Ground measurements of the shock wave noise from supersonic bomber airplanes in the altitude range from 30,000 to 50,000 feet [NASA TN D-880]
By: Maglieri, Domenic J.
Contributor(s): Hubbard, Harvey H.
Material type:
BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D. C. NASA 1961Description: 24p.Subject(s): Supersonic planes
Contents:
Technical note D-880
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | Not for loan | 65488 [D-880] |
Total holds: 0
Technical note D-880
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